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A340-600
GENERAL
REV 19
SEQ 001
0.00
IMPORTANT
SCOPE
The QRH contains some specific procedures which are not displayed on ECAM.
As
a general
rule,
procedures displayed on the ECAM are not provided in the QRH
(refer
to FCOM
3.02).
TASK SHARING FOR ABN/EMER PROC
For all abnormal/emergency procedures the task sharing is as follows:PF - Pilot Flying - responsible for: Thrust levers
• Flight path and airspeed control
• Aircraft configuration (Request configuration change)
• Navigation
• Communications
PNF - Pilot Non-Flying - responsible for:-
R
• ECAM or checklist reading
• Execution of required actions on PF request
• Engine master switches, ENG FIRE pb (with consent of PF)
ECAM CLEAR
DO NOT CLEAR ECAM WITHOUT CROSS-CONFIRMATION OF BOTH PILOTS.
ABN/EMER PROC INITIATION
R
Procedures are initiated on pilot flying command.
No action will be taken (apart from audio warning cancel through MASTER WARN
light) until:-
R
R
R
R
R
• The appropriate flight path is established and,
• The aircraft is at least 400 feet above the runway, if a failure occurs during takeoff,
approach, or go-around.
(In some emergency cases, provided the appropriate flight path is established, the
pilot flying may initiate actions before this height).
NORMAL CHECKLIST
The Before Start, After Start, Parking and Securing Aircraft checklists will be
initiated by the CM1 and read by the CM2. Other Normal checklists are initiated
by the PF and read by the PNF.
The Before T.O. checks, below the line, and after landing checks, when requested,
should be actioned silently by the PNF as listed in the FCOM 3, SOPs. After
completion of the actions, the Table or QRH checklist should be read aloud
confirming the actions and the appropriate "........ checklist complete" announced by
the PNF.
The appropriate crew member shall respond after having checked the existing
configuration. When both pilots have to respond, "BOTH" is indicated.
The sign or indicates the specific VIRGIN ATLANTIC AIRWAYS requirements.
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A340-600
GENERAL
REV 23
SEQ 001
0.00A
USE OF SUMMARIES
GENERAL
In case of an electrical emergency configuration, or a dual hydraulic failure:
The ECAM should be applied first.
This includes both the procedure, and the STATUS section.
Only after announcing "ECAM ACTIONS COMPLETED", should the PNF refer to the
corresponding QRH summary.
When the failure occurs, and after performing the ECAM actions, the PNF should
refer to the "CRUISE" portion of the summary, in order to determine the landing
distance coefficient.
Since normal landing distances are also given on this page, the PNF will be able to
compute the landing distance taking failure(s) into account, in order for the pilot to
decide whether to divert or not.
APPROACHPREPARATION
As always, approach preparation includes a review of the ECAM STATUS.
After reviewing the STATUS, the PNF should refer to the "CRUISE" portion of the
summary, to determine the VREF correction, and compute the VAPP.
A VREF table is provided in the summary, for failure cases leading to the loss of the
MCDU.
The LANDING and GO-AROUND portions of the summary should be used for the
approach briefing.
APPROACH
The APPR PROC actions should be performed by reading the APPROACH portion
of the summary.
The PNF should then review the ECAM STATUS, and check that all the APPR
PROC actions have been completed.
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A340-600
AWOPS / AUTOLAND
REV 00
0.00B
SEQ VAA
SUMMARY
NB:
This is a summary of the A340 AWOPS procedures to be used when Low Visibility
Operations are announced - for the full text please refer to the the FCOM and Ops Manual.
LOW VISIBILITY TAKE-OFF
1.
2.
3.
4.
5.
6.
7.
8.
9.
Return Alternate required within 2 hours, Cat 1 or above.
Check H.I. edge and C/L lighting available.
Check threshold and R/W end lighting available.
Check T/O minima.
All relevant RVR's at or above minima.
Maximum crosswind 10 kts.
TOGA thrust to be used.
Verify ILS tuned on RAD NAV page (LS pb ON).
Check lights visible 9/5 for spacing 15 m / 30 m with RVR 125 m.
RTO
- Max autobrake.
- Maintain C/L.
- Call ATC.
- 900 m to go : C/L lights to alternating red/white.
- 300 m to go : C/L lights on red.
LANDING IN CAT 2/3
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
A/C autoland operative. Check Tech Log and QRH page.
Airfield equipment to Cat 2/3 standard (FCOM 2 + NOTAMS/ATIS).
(a) Both pilots to hold valid LVO certificates.
( b) Capt. as PF.
Confirm runway approved for autoland (No Cat 3B on L status runways).
Minima checked.
Two alternates required Cat 1 and above.
Extra fuel for holding/approach delays (normally > 45 mins).
Autoland wind limits (30 kt HWC, 10 kt TWC, 20 kt XWC).
Use config "full" (config 3 - one engine inoperative).
Approach briefing to include:
(a) Callouts on approach.
(b) Different PF/PNF duties.
(c) R/W and approach lighting expected.
(d) Visual cues at DH.
(e) Procedures for Rollout, R/W clearance and taxi.
( f ) GA procedure.
(g) Alternates and fuel state.
(h) Seat position.
(j)
(k)
Aircraft external lighting.
Autobrake 3 unless runway length or surface conditions warrant 4.
APPROACH
- APPR selected - select second A/P, check category.
- TD or mid-point RVR below minima - continue to OM or equivalent.
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REV 00
A340-600
AWOPS / AUTOLAND
SEQ VAA
0.00C
OM OR EQUIVALENT
- RVR's must be at or above minima.
- MID PT RVR may be substituted if T/D RVR is not available.
- STOP END RVR is advisory.
1000' AAL
- PNF calls "1000 ft G/A ALT set".
-PF calls "Check".
500' RADIO
- PNF calls "500 feet radio".
-PF calls "Check".
350' RADIO / LAND GREEN ANNUNCIATED
- PF and PNF check ILS course on PFD
- PNF calls "LAND green".
-PF calls "Course checked".
DH + 100'
- Autocall - PNF calls "One hundread above"
- PF responds "Check".
DH
-Auto Call-PNF calls "Minimum"
-PF responds "Landing" or "G/A Flap".
If visual reference lost below DH - Go-Around.
40'R
PNF check 'FLARE' annunciated - call "NO FLARE" if not.
10'R
Autocall "RETARD". PF closes thrust levers.
GO-AROUND
Thrust levers to 'TO GA' - A/P commands G/A.
AFTER LANDING
Report 'runway vacated' when the entire aircraft is clear of CAT 3 protected area.
NON-NORMAL PROCEDURES
- Carry out a GA if following occurs:
Below 1000 ft and 200 ft:
Capability decrease (click, click, click).
Amber Caution plus single chime.
No 'LAND' green by 350 ft / incorrect RWY course.
Engine failure.
AP off (cavalry charge).
200ft or below
Red autoland light.
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PRM BREAKOUT MANOEUVRE
A340-600
REV 00
SEQ VAA
0.00D
Initial Actions
PF
1)
2)
Disengage A/P
Looking through F/D, turn immediatly towards cleared heading then
initiate climb/descent if or as required.
1)
2)
Acknowledge
Select cleared heading/ALT and pull.
PNF
Subsequent actions
When appropriate, clean up as required. eg a standard G/A procedure can
be initiated by PF selecting TOGA then back to CL, then calling G/A Flaps.
CAUTIONS
1)
Do not overbank. The necessity to immediately respond is ad
dressed by disconnecting A/P then smoothly applying bank, looking
through F/D.
2)
Beware of high ROD beyond 1000 fpm in event of descending
breakout. Consider that ROD will already be approx 800 fpm, if
established on G/S.
3)
Do not descend below cleared altitude.
1)
It is recommended to initially target the following pitch altitudes
Climbing
+12 deg.
Descending +2 deg. (or current attitude if stablised on G/S.)
Then adjust as required.
2)
A/THR will maintain SPEED mode. brief accordingly if A/THR U/S.
3)
If simultaneous TCAS RA, turn with ATC, climb/descend with TCAS.
Notes
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A340-600
AWOPS / AUTOLAND
REV 00
SEQ VAA
0.00E
1 EMERGENCY PROCEDURES
ELEC
• ELEC EMER CONFIG-SYS REMAINING ................................................ 1.01
• ELEC EMER CONFIG Summary ............................................................ 1.03
FIRE
• SMOKE/FUMESREMOVAL..................................................................... 1.04
• SMOKE/FUMES/AVNCS SMOKE ............................................................ 1.05
HYDRAULIC
• HYD B+Y SYS LO PR Summary ............................................................. 1.07
• HYD G+B SYS LO PR Summary ............................................................ 1.08
• HYD G+Y SYS LO PR Summary ............................................................ 1.09
LANDING GEAR
• LOSS OF BRAKING ................................................................................ 1.10
NAVIGATION
••
GPWS/EGPWS
....................................................................1.11
TCAS
WARNINGS ALERTS
.............................................................................1.12
POWER PLANT
• ALL-ENGINE FLAMEOUT-FUEL REMAINING ........................................ 1.13
• ALL-ENGINE FLAMEOUT-NO FUEL REMAINING ................................. 1.17
• TWO ENGINE INOP LANDING ............................................................... 1.20
MISCELLANEOUS
• DITCHING ............................................................................................... 1.21
• FORCED LANDING ................................................................................ 1.23
• EMER DESCENT .................................................................................... 1.25
• CABIN FIXED OXYGENSYSTEM ............................................................ 1.26
• ON GROUND EMER/EVACUATION ....................................................... 7.01
2 ABNORMALPROCEDURES
AUTO FLT
• LOSS OF FMS DATA IN DESCENT/APPROACH
(SEVERE RESET) ................................................................................ 2.00B
• MCDU FAILURE ..................................................................................... 2.01
EQUIPMENT
• COCKPIT DOOR FAULT ........................................................................ 2.01
F/CTL
• RUDDER JAM/RUDDER PEDAL JAM .................................................... 2.02
• RUDDER TRIM RUNAWAY .................................................................... 2.03
• LDG WITH FLAPS/SLATS JAMMED ...................................................... 2.05
••
NO
FLAPS
NO SLATS
LANDING
.......................................................... 2.06A
LOW
ENERGY
WARNING
......................................................................
2.06
FUEL
• FUEL LEAK ............................................................................................. 2.07
• GRAVITY FUEL FEEDING .................................................................... 2.08A
• WING TK IMBALANCE ............................................................................ 2.08
• FUEL JETTISON ..................................................................................... 2.09
• TRIM TANK FUEL UNUSABLE ............................................................... 2.10
• FUEL LO TEMP..................................................................................... 2.10A
continued/ICE AND RAIN PROTECTION
VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006
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A340-600
QRH INDEX
REV 00
SEQ VAA
0.00F
2 ABNORMAL PROCEDURES (continued)
ICE AND RAIN PROTECTION
• DOUBLE STAT (AOA) HEAT FAILURE ................................................... 2.11
INDICATING/RECORDING
• DISPLAY UNIT FAILURE ........................................................................ 2.11
• ECAM SINGLE DISPLAY ........................................................................ 2.11
• TAILSTRIKE .......................................................................................... 2.11A
• DISPLAY DISCREPANCY....................................................................... 2.12
LANDING GEAR
• L/G GRAVITY EXTENSION ..................................................................... 2.13
• LDG WITH ABNORMAL CENTER L/G .................................................... 2.14
• LDG WITH ABNORMAL NOSE/MAIN L/G ............................................... 2.15
• RESIDUAL BRAKING PROC .................................................................. 2.17
NAV
• FM/GPS POS DISAGREE ............................................................................... 2.18
• ADR 1+2+3 FAULT ................................................................................. 2.19
• ADR DISAGREE ..................................................................................... 2.20
• ADR CHECK PROC ........................................................................................ 2.20A
• UNRELIABLE SPEED INDICATION ....................................................... 2.21
• IR ALIGNMENT IN ATT MODE ................................................................ 2.24
POWER PLANT
• ENG RELIGHT IN FLIGHT ...................................................................... 2.26
• ENG STALL ............................................................................................. 2.27
• HIGHENGINE VIBRATION ..................................................................... 2.28
• ENGINE TAILPIPE FIRE ......................................................................... 2.28
MISCELLANEOUS
• OVERWEIGHT LANDING ...................................................................... 2.29
• COCKPIT WINDSHIELD/WINDOW CRACKED ..................................... 2.30
• COCKPIT WINDSHIELD/WINDOW ARCING ......................................... 2.30
• VOLCANIC ASH ENCOUNTER .............................................................. 2.30
• BOMB ON BOARD .................................................................................. 2.31
• RESET OF COMPUTERS ....................................................................... 2.35
• ECAM ADVISORYCONDITIONS ............................................................ 2.38
• VAPPDETERMINATION ............................................................................ 2.40
• LDG CONF/APP SPD/LDG DIST FOLLOWING FAILURES ................... 2.41
3 NORMAL PROCEDURES
•
•
•
•
•
SAFETY EXTERIOR INSPECTION ......................................................... 3.01
PRELIMINARY COCKPIT PREPARATION ............................................ 3.01
AFTER LANDING .................................................................................... 3.02
PARKING ................................................................................................ 3.02
SECURING THE AIRCRAFT .................................................................. 3.02
continued/4
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A340-600
QRH INDEX
REV 00
SEQ VAA
0.00G
4 IN-FLIGHT PERFORMANCE
•
•
•
•
•
•
•
•
•
SPEEDS ................................................................................................. 4.01
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF 3 ..................... 4.02
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF FULL .............. 4.03
AUTOLAND LANDING DISTANCE WITH AUTOBRAKE ......................... 4.04
ENG OUT
MAX ALTITUDE (ONE or TWO or THREE ENGINES OUT) .................... 4.05
GROSS FLIGHT PATH DESCENT AT GREEN DOT SPEED ................. 4.06
LONG RANGE CRUISE .......................................................................... 4.07
IN CRUISE QUICK CHECK .................................................................... 4.08
ALL ENGINES:
CLIMB CEILING ...................................................................................... 4.09
MAX/OPT ALTITUDE ............................................................................... 4.10
IN CRUISE QUICK CHECK ................................................................... 4.11
COST INDEX .......................................................................................... 4.12
DESCENT .............................................................................................. 4.13
DIVERSION............................................................................................ 4.14
FLIGHT WITHOUT CAB PRESS ............................................................. 4.15
GROUND DISTANCE/AIR DISTANCE CONVERSION ........................... 4.16
IAS MACH CONVERSION ....................................................................... 4.17
5 OPS DATA
•
•
•
•
SEVERE TURBULENCE ........................................................................ 5.01
HYD ARCHITECTURE ........................................................................... 5.02
FLT CTL ARCHITECTURE ..................................................................... 5.03
REQUIRED EQUIPMENT FOR CAT 2 AND CAT 3................................. 5.04
6
OEB
7
NORMAL CHECKLIST
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QRH INDEX
A340-600
4
PAGE
VS
0.00H
IN-FLIGHT PERFORMANCE
•
SPEEDS ..................................................................................................4.01
•
•
•
•
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF 3 ........................ 4.02
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF FULL ................. 4.03
AUTOLAND LANDING DISTANCE WITH AUTOBRAKE............................ 4.04
ENG OUT
MAX ALTITUDE (ONE or TWO or THREE ENGINES OUT) ...................... 4.05
GROSS FLIGHT PATH DESCENT AT GREEN DOT SPEED ................... 4.06
LONG RANGE CRUISE ............................................................................ 4.07
IN CRUISE QUICK CHECK ...................................................................... 4.08
ALLENGINES:
CLIMBCEILING ........................................................................................ 4.09
MAX/OPT ALTITUDE ................................................................................ 4.10
IN CRUISE QUICK CHECK ..................................................................... 4.11
COST INDEX ............................................................................................ 4.12
DESCENT ............................................................................................... 4.13
•
•
•
•
5
VAA
DIVERSION ............................................................................................. 4.14
FLIGHT WITHOUT CAB PRESS .............................................................. 4.15
GROUND DISTANCE/AIR DISTANCE CONVERSION.............................. 4.16
IAS MACHCONVERSION .........................................................................4.17
OPS DATA
•
•
•
•
SEVERE TURBULENCE .......................................................................... 5.01
HYD ARCHITECTURE .............................................................................. 5.02
FLT CTL ARCHITECTURE ....................................................................... 5.03
REQUIRED EQUIPMENT FOR CAT 2 AND CAT 3 ................................... 5.04
6
OEB
7
NORMAL CHECKLIST
VIRGIN ATLANTIC AIRWAYS REVISION 06 / 12 March 2004
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A340-600
R
R
EMERGENCY PROCEDURES
REV 24
1.00
SEQ 001
ELEC
• ELEC EMER CONFIG-SYS REMAINING . . . . . . . . . . . . . . . .
• ELEC EMER CONFIG Summary . . . . . . . . . . . . . . . . . . . . . .
1.01
1.03
FIRE
• SMOKE /FUMES REMOVAL . . . . . . . . . . . . . . . . . . . . . . . .
• SMOKE/FUMES/AVNCS SMOKE . . . . . . . . . . . . . . . . . . . . .
1.04
1.05
HYDRAULIC
• HYD B+Y SYS LO PR Summary . . . . . . . . . . . . . . . . . . . . . .
• HYD G+B SYS LO PR Summary . . . . . . . . . . . . . . . . . . . . . .
• HYD G+Y SYS LO PR Summary . . . . . . . . . . . . . . . . . . . . . .
1.07
1.08
1.09
LANDING GEAR
• LOSS OF BRAKING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1.10
NAVIGATION
R
R
R
R
R
VI6 ALL
• GPWS/EGPWS
ALERTS . . . . . . . . . . . . . . . . . . . . . . . .
• TCAS WARNINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1.11
1.12
POWER PLANT
• ALL ENG FLAMEOUT-FUEL REMAINING . . . . . . . . . . . . . . .
• ALL ENG FLAMEOUT-NO FUEL REMAINING . . . . . . . . . . . .
• TWO ENGINES INOP LANDING . . . . . . . . . . . . . . . . . . . . . .
1.13
1.17
1.20
MISCELLANEOUS
• DITCHING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FORCED LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• EMER DESCENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• CABIN FIXED OXYGEN SYSTEM . . . . . . . . . . . . . . . . . . . . .
• ON GROUND EMER/EVACUATION . . . . . . . . . . . . . . . . . . .
1.21
1.23
1.25
1.26
7.01
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A340-600
EMERGENCY PROCEDURES
ELEC EMER CONFIG
SYS REMAINING
PRESS AUTO SYS 1
COM
EIS
EMER
EQPT
FLT INS
FIRE
R
EMER GEN RUNNING
SUPPLIED
SUPPLIED
BY ENG
BY RAT
HYD PUMPS
1.01
BAT ONLY
IN FLT
ON GND
(IAS < 50 kt)
Norm
Norm
Norm
inop
Norm
inop
Norm
inop
Norm
Norm
Norm
Norm
Norm
Norm
Norm
AVIONIC VENT
OVBD only
OVBD only
CARGO VENT
OVBD only OVBD only
ISOL valve only
inop
inop
inop
MCDU
1 only
inop
inop
3 only
FCU
1 only
1 only
1 only
1 only
VHF 1
Norm
Norm
Norm
Norm
RMP 1
Norm
Norm
Norm
Norm
ACP (CAPT., F/O)
Norm
Norm
Norm
Norm
CIDS
Norm
Norm
Norm
Norm
INTERPHONE
CVR
Norm
Norm
Norm
inop
Norm
inop
Norm
inop
LOUDSPEAKER 1 + 2
Norm
Norm
Norm
Norm
PFD 1
Norm
Norm
Norm
Norm
ECAM upper DU
Norm
Norm
Norm
Norm
DMC 1 or 3
Norm
Norm
Norm
Norm
SDAC 1, FWC 1
Norm
Norm
Norm
Norm
ECP
Norm
Norm
Norm
Norm
CREW OXY valve ctl
Norm
inop
inop
inop
PAX OXY
Norm
Norm
Norm
Norm
SLIDES ARM/WARN
Norm
Norm
Norm
Norm
CLOCK
ENG LOOPS
Norm
A only
Norm
A only
Norm
A only
Norm
A only
APU LOOP
A only
A only
A only
Norm
CARGO SMOKE DET
1 only
inop
inop
inop
ENG FIRE EXT.
Bottle 1
Bottle 1
Bottle 1
Bottle 1
APU FIRE EXT.
Bottle 1
Bottle 1
Bottle 1
Bottle 1
CARGO FIRE EXT.
Bottle 1
Bottle 1
Bottle 1
Bottle 1
APU AUTO EXT.
FLT
CTL
SEQ 100
Norm
AIR COND MAN PRESS CTL
RAM AIR
PRESS
PACK VALVE
VENT
AUTO FLT
REV 19
-
-
-
Norm
PRIM 1
Norm
Norm
Norm
Norm
SEC 1
Norm
Norm
Norm
Norm
FCDC
Norm
inop
inop
inop
1 only *
1 only *
1 only *
inop
1 only *
inop
1 only *
inop
PITCH TRIM
1 only
inop
inop
inop
RUDD TRIM
1 only ****
inop
inop
inop
SFCC SLATS
SFCC FLAPS
* Operative when LAND RECOVERY pushbutton is ON.
**** RUDDER TRIM is operative, but position indicator is lost on center pedestal.
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EMERGENCY PROCEDURES
A340-600
REV 22
SEQ 200
ELEC EMER CONFIG
SYS REMAINING
EMER GEN RUNNING
SUPPLIED
SUPPLIED
BY ENG
BY RAT
HYD PUMPS
1.02
BAT ONLY
IN FLT
ON GND
(IAS < 50 kt)
FCMC
1 only
Inop
Inop
1 only
FDC
PUMPS
Norm
PUMP*****
2
Norm
inop
Norm
inop
X FEED
Norm
*****
PUMP 2 and
LT.TK PUMP
Mot 1 only
Mot 1 only
inop
inop
LP VALVES
Mot 1 only
Mot 1 only
Mot 1 only
Mot 1 only
APU, ISOL VALVES
Norm
Norm
Norm
Norm
APU PUMP
Norm
Norm
Norm
Norm
APU LP VALVE
Norm
Norm
Norm
Norm
FUEL
Inop
inop
inop
inop
FIRE SOV
JETTISON
Norm
Norm
Norm
Norm
RAT CTL
Norm
Norm
Norm
Norm
ICE &
ENG A. ICE
Open
Open
Open
Open
RAIN
CAPT PITOT
Norm
Norm
Norm
Norm
RAIN REPEL
Capt
Capt
Capt
Capt
HYD
LGCIU
L/G
1 only *
1 only *
1 only *
1 only *
GRVTY EXT
Norm
Norm
Norm
Norm
IND. PANEL
Norm
Norm
Norm
Norm
inop
inop
inop
inop
AUTO BRK/ANTI SKID
NAV
OXYGEN
PARK BRK
Norm
Norm
Norm
Norm
IR 1 and 3
Norm
Norm
Norm
Norm
IR 2
5 min
5 min
5 min
5 min
ADR 1 or 3
Norm
Norm
Norm
Norm
** VOR or ADF
1 only
1 only
1 only
1 only
MMR
1 only
1 only
1 only
1 only
DDRMI
Norm
Norm
Norm
Norm
ATC
ISIS
1 only
Norm
Inop
Norm
Inop
Norm
Inop
Norm
Crew Oxy valve ctl
Norm
inop
inop
inop
Pax Oxy
Norm
Norm
Norm
Norm
BMC 1 + 4
inop
man only
BMC 1 + 4
inop
man only
BMC 1 + 4
inop
man only
BMC 1 + 4
inop
man only
Norm
ENG BLEED
PNEU
X BLEED
APU
Norm
Norm
Norm
SLIDES ARMWARN
Norm
Norm
Norm
Norm
FADEC
A only
A only
A only
A only
PWR
IGNITION
A only
A only
A only
A only
PLT
REV
DOORS
HP VALVE closure
inop
inop
inop
inop
Norm
Norm
Norm
Norm
*
**
Operative when the LAND RECOVERY pushbutton is ON.
Only VOR1 or ADF1 (as selected on the DDRMI) is available at a time.
If the DDRMI is deactivated, only VOR1 is available on the ND (ADF1 will not be available
R
R
independently of the selection performed on the DDRMI).
*** Shed when LAND RECOVERY ON.
*****. All crossfeed valves automatically open.
.
If Pump 1 is inoperative, Pump 4 STBY takes over.
Remaining pump is lost, when the LAND RECOVERY pushbutton is ON.
When supplied by the RAT only, the remaining pump is lost when speed is below 260 knots.
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A340-600
EMERGENCY PROCEDURES
REV 25
1.05
SEQ 001
SMOKE/FUMES/AVNCS SMOKE
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
LAND ASAP
APPLY IMMEDIATELY
- VENT EXTRACT . . . . . . . . . . . . . . . . . . . . . . . OVRD PNF
- CAB FANS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
- GALLEYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
PNF
PNF
PNF
- CKPT/CAB COM . . . . . . . . . . . . . . . . . . ESTABLISH
PNF
IF REQUIRED :
- CREW OXY MASKS . . . . . . . . . . ON/100%/EMERG BOTH
IF SMOKE SOURCE IMMEDIATELY OBVIOUS,
ACCESSIBLE AND EXTINGUISHABLE :
- FAULTY EQUIPT. . . . . . . . . . . . . . . . . . . . . . ISOLATE PNF
IF SMOKE SOURCE NOT IMMEDIATELY
ISOLATED :
- DIVERSION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE
- DESCENT (FL 100/MEA, min obstacle clearance
altitude) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE
At ANY TIME of the procedure, if smoke/fumes
becomes the GREATEST THREAT:
-
SMOKE/FUMES REMOVAL . . . . . . . . . . . . .CONSIDER
ELEC EMER CONFIG . . . . . . . . . . . . . . . . . .CONSIDER
Refer to the end of the procedure to set ELEC EMER
CONFIG.
At ANY TIME of the procedure, if situation
becomes UNMANAGEABLE:
-
IMMEDIATE LANDING . . . . . . . . . . . . . . . . . .CONSIDER
R
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A340-600
EMERGENCY PROCEDURES
REV 25
SEQ 100
1.06
SMOKE/FUMES/AVNCS SMOKE (CONT'D)
R
If AIR COND SMOKE SUSPECTED:
- APU BLEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
R
VENT EXTRACT . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO
PACK 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
If smoke continues:
- PACK 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
- PACK 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
If smoke still continues:
- PACK 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
- VENT EXTRACT. . . . . . . . . . . . . . . . . . . . . . . . . OVRD
-
SMOKE/FUMES REMOVAL . . . . . . . . . . . . CONSIDER
IF CAB EQUIPMENT SMOKE SUSPECTED :
- PAX SYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
If smoke continues
- EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . . . . .ON
- COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
- SMOKE DISSIPATION . . . . . . . . . . . . . . . . .CHECK
R
- FAULTY EQPT . . . . . . . . . . . . .SEARCH/ISOLATE
If smoke still continues or when faulty
equipment confirmed isolated :
- COMMERCIAL . . . . . . . . . . . . . . . . . . . . . .NORM
- PAX SYSTEM . . . . . . . . . . . . . . . . . . .NORM
- SMOKE/FUMES REMOVAL . . . . . CONSIDER
R
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A340-600
EMERGENCY PROCEDURES
REV 25
SEQ 300
1.09
HYD G + Y SYS LO PR Summary
C
R
R
R
R
R
R
R
SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT USE
MAX SPD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 305/.82
MANEUVER WITH CARE
ALTN LAW : PROT LOST
FUEL : Increased fuel comsumption
LANDING CONF
APPROACH SPEED
LANDING DIST
MULTILY BY
R
U
I
S
: Use FLAP 2
E If flaps < 1+F
If 1+F < Flaps < 2 : Use FLAP 2
VAPP = VREF+40
VAPP = VREF+15
If Flaps = 2
: Use FLAP 3 VAPP = VREF+10
If 2 < Flaps < 3 : Use FLAP 3 VAPP = VREF+10
If Flaps > 3 : Use FLAP FULL VAPP = VREF+10
DRY
WET
CONTA
1.65
1.40
1.35
1.35
1.35
2.15
1.75
1.70
1.70
1.70
2.30
1.95
1.85
1.85
1.85
SLATS SLOW / FLAPS JAMMED
CAT 1 ONLY
A GPWS SLAT MODE (If Flaps< 2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
P
Slat extension : SPD SEL . . . . . . . . . . . . . . . . . . . . . . . . . . VFE NEXT - 5 KT
P For
R When in landing CONF : DECELERATE TO CALCULATED VAPP
L/G GRAVITY EXTENSION :
MAX SPD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 250 KT
180
200
220 240 260 280 300
320 340 360 380
13% CG
132
133
139 146 151 157 163
168 173 178 183
35% CG
132
133
135 142 147 153 159
164 169 174 179
W (1000 KG)
VREF = VLS
CONF FULL
L
A
N
D
I
N
G
FLARE : Only one ELEV and 2 spoilers per wing.
A/C slightly sluggish - Direct law
SPOILERS : Only 2 per wing
REVERSERS : Only N° 2
BRAKING : ALTERNATE
NO NOSEWHEEL STEERING
G
NO GEAR RETRACTION. INCREASED FUEL CONSUMPTION
O
R
A
R
R O
U
R N
D
For circuit : MAINTAIN SLATS/FLAPS CONFIGURATION
Recommended speed : MAX SPD - 10 KT/250 KT
For diversion :
If Flaps at zero : SELECT CLEAN CONFIGURATION
Normal operating speeds (MAX SPD 250 KT)
If Flaps not at zero : MAINTAIN SLATS/FLAPS CONFIG
Recommended speed : MAX SPD - 10 KT/250 KT
ACTUAL LANDING DISTANCES (feet) (for contaminated runways, refer to 4.03)
WEIGHT (1000 KG)
DRY runway
WET runway
180
3320
4690
CORRECTIONS
DRY runway
WET runway
205 230 255 280
305 330 355 380
3420 3720 4080 4470 4900 5400 6050 6740
4920 5500 6120 6690 7330 7960 8600 9220
+ 1000 ft above SL
+4%
+ 10 Kt tailwind
+ 16 %
+ 23 %
The method for approach speed computation is given in the QRH 2.40.
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A340-600
EMERGENCY PROCEDURES
REV 21
1.10
SEQ 100
LOSS OF BRAKING
IF AUTOBRAKE IS SELECTED:
– BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . PRESS
IF NO BRAKING AVAILABLE:
– REV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX
– BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . RELEASE
– A/SKID . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
– BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . PRESS
– MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 PSI
IF STILL NO BRAKING
– PARKING BRAKE . . . . . . . . . . . . . . . . . . SHORT AND
SUCCESSIVE APPLICATION
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A340-600
EMERGENCY PROCEDURES
REV 25
1.11
SEQ 102
EGPWS ALERT
CAUTION
During night or IMC conditions, immediately apply the procedure. Do not
delay reaction for diagnosis.
During daylight VMC conditions, with terrain and obstacles clearly in sight,
the alert may be considered cautionary. Take positive correction action,
until the alert ceases or a safe trajectory is ensured.
"PULL UP" - "TERRAIN TERRAIN PULL UP"- "TERRAIN AHEAD
PULL UP" - "OBSTACLE AHEAD PULL UP":
Simultaneously:
R
R
R
— A/P . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
— PITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL UP
Pull up to full backstick and maintain.
— THRUST LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TOGA
— SPEED BRAKE LEVER . . . . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED
— BANK . . . . . . . . . . . . . . . . . . .WINGS LEVEL TO INITIATE PULL UP
THEN ADJUST AS RQRD
When the flight path is safe, and the GPWS warning ceases:
Decrease pitch attitude and accelerate.
When speed is above VLS, and vertical speed is positive :
Clean up aircraft, as required.
"TERRAIN TERRAIN" - "TOO LOW TERRAIN" :
Adjust the flight path, or initiate a go-around.
"TERRAIN AHEAD" - "OBSTACLE AHEAD" - "CAUTION
OBSTACLE":
Adjust the flight path. Stop descent. Climb and/or turn, as necessary,
based on analysis of all available instruments and information.
"SINK RATE" "DON'T SINK" :
Adjust pitch attitude and thrust to silence the alert.
"TOO LOW GEAR" - "TOO LOW FLAPS" :
Correct the configuration, or perform a go-around.
"GLIDESLOPE" :
Establish the airplane on the glideslope, or switch OFF the G/S mode
pushbutton, if flight below the glideslope is intentional (non-precision
approach).
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A340-600
EMERGENCY PROCEDURES
REV 23
SEQ 100
1.12
NAV TCAS WARNINGS
Traffic Advisory: "TRAFFIC" messages:
— Do not manoeuvre based on a TA alone.
— Attempt to see the reported traffic.
Preventive Resolution Advisory: "MONITOR VERTICAL SPEED"
messages:
— Maintain or adjust the vertical speed, as required, to avoid the red area
of the vertical speed scale.
— Notify ATC.
— When "CLEAR OF CONFLICT" is announced:
Resume normal navigation, in accordance with ATC clearance.
Corrective Resolution advisory: All "CLIMB" and "DESCEND" or
"MAINTAIN VERTICAL SPEED MAINTAIN" or "ADJUST VERTICAL
SPEED ADJUST" type messages:
— Respond promptly and smoothly to an RA.
— A/P (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
— BOTH FDs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Adjust the vertical speed, as required, to that indicated on the green area
of the vertical speed scale.
NOTE: Avoid excessive manoeuvres while aiming to keep the vertical
speed just outside the red area of the VSI and within the green
area. If necessary, use the full speed range between Vα max
and Vmax.
— Respect stall, GPWS or windshear warning.
—
— Notify
When ATC.
"CLEAR OF CONFLICT" is announced:
• Resume normal navigation in accordance with ATC clearance.
• A/P/FD can be re-engaged as desired.
GO-AROUND procedure must be performed when an RA "CLIMB"
or "INCREASE CLIMB" is triggered on final approach
NOTE : Resolution Advisories (RA) are inhibited below 900 feet
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A340-600
EMERGENCY PROCEDURES
REV 24
SEQ 205
1.15
ENG ALL ENG FLAMEOUT - FUEL REMAINING Cont'd
IF FORCED LANDING ANTICIPATED
APPROACH
— MIN RAT SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .140 KT
At a suitable altitude (not below 3000 feet AGL), configure the
aircraft for landing (CONF 1; L/G DOWN)
— LAND RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT
EMER GEN is lost at slats' extension. The aircraft is supplied by batteries only.
At slat extension, if FUEL MAN FWD XFR has been selected
— T TANK MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO
— T TANK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
— MAX SPEED for GRAVITY EXTENSION . . . . . . . . . . . . . . . .250 KT
— L/G GRAVTY EXTN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
Disregard "USE MAN PITCH TRIM" on the PFD, because the stabilizer is frozen in the
position it was at, when the windmilling was insufficient to provide hydraulic power.
When L/G downlocked
— L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
— APPROACH SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . 190 KT
Adjust the speed to the Vapp given above. However, to reach the landing field/runway,
the approach speed may be adjusted up to 250 knots (max speed with landing gear
extended)
— GND SPLR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARM
— MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1000 PSI
AT 1000 FEET AGL
— CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"
AT
200 FEET
— BRACE
FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"
AT TOUCHDOWN
— ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— APU MASTER SW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— BRAKES ON ACCU ONLY
AFTER LANDING
When the aircraft has stopped :
— PARKING BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
— ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
— FIRE pushbutton (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . .PUSH
— AGENTS (ENG and APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DISCH
— EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE
— BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING
If not, switch on the transmitter
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A340-600
EMERGENCY PROCEDURES
REV 25
SEQ 205
1.16
ENG ALL ENG FLAMEOUT- FUEL REMAINING Cont'd
IF DITCHING ANTICIPATED
APPROACH
— MIN RAT SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .140 KT
At a suitable altitude (not below 3000 feet AGL), configure the
aircraft for ditching (CONF 1, L/G UP)
— LAND RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT
EMER GEN is lost at slats' extension. The aircraft is supplied by batteries only.
At slat extension, if FUEL MAN FWD XFR has been selected
— T TANK MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO
— T TANK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
— L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK UP
— APPROACH SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . .190 KT
AT 1000 FEET AGL
— CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"
— DITCHING pushbutton . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
In case of strong crosswind, ditch face to the wind.
In the absence of strong crosswind, prefer ditching parallel to the swell. Touchdown
with approximately 11 degrees of pitch and minimum aircraft vertical speed.
AT 200 FEET
— BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"
R
R
AT TOUCHDOWN
— ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— APU MASTER SW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
R
AFTER DITCHING
— ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
— FIRE pushbutton (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . .PUSH
— AGENTS (ENG and APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DISCH
— EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE
— BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING
If not, switch on the transmitter
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A340-600
EMERGENCY PROCEDURES
REV 25
SEQ 104
1.17
ENG ALL ENG FLAMEOUT - NO FUEL REMAINING Cont'd
This paper procedure is applicable in the case of an all engine flameout, if no fuel
remains on board. It includes all the necessary and sufficient ECAM steps and additional
information to manage the situation. Therefore, the flight crw should apply this paper
procedure and then, if time permits, clear ECAM warnings and check the ECAM STATUS
page.
— RAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAN ON
— THRUST LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
— OPTIMUM SPEED . . . . . . . . . . . . . . . . . . . 220 KT/GREEN DOT
Initially, fly 220 knots, because the Captain's PFD does not display the green dot speed.
When time permits, check the green dot value in the following table :
GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS)
Weight
At or below
FL 200
FL 300
FL 400
(1000 kg)
FL 100
280
232
247
260
246
260
224
238
252
245
240
216
230
243
241
220
208
221
234
233
200
200
211
223
221
180
190
199
210
208
At green dot speed, the aircraft can fly up to approximately 3 NM per
1000 feet (with no wind).
Average rate of descent is approximately 1500 feet/min.
— LANDING STRATEGY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DETERMINE
Determine if a runway can be reached, or determine the most appropriate place for a
forced landing/ditching.
— EMER ELEC POWER if not automatically coupled) . . . . . MAN ON
— VHF 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .USE
Only VHF1 is always supplied. Notify ATC of the nature of the emergency and state
intentions. If there is no contact with the ATC, transmit a distress message on VHF
frequency 121.5 MHz.
— Cabin
CREW
altitude
OXY
willMASKS
increase due
(Above
to the lack
FL of
100)
engine
. . bleed
. . . . :. The
. . . EXCESS
. . . . . . CAB
. . . .ON
ALT
ECAM warning could be triggered. Depending on the situation, to gain gliding distance,
the flight crew may disregard the ECAM emergency descent requirement, because
passengers will be provided with oxygen for a sufficient period of time.
— CABIN AND COCKPIT . . . . . . . . . . . . . . . . . . . . . . . . . .PREPARE
— Loose equipment secured
— Survival equipment prepared
— Belts and shoulder harnesses locked
R
— SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— USE RUDDER WITH CARE
WHEN BELOW FL 150 :
— RAM AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
Switch ON the RAM AIR to ensure complete depressurization.
APPROACH PREPARATION
— BARO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SET
— CREW MASKS/OXY SUPPLY (below FL 100) . . . . . . . . . . . . . .OFF
NOTE : Final descent slope, when configured (CONF 1 ; L/G DOWN), will be approximately
650 feet/NM (with no wind),
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A340-600
EMERGENCY PROCEDURES
REV 24
SEQ 205
1.18
ENG ALL ENG FLAMEOUT - NO FUEL REMAINING Cont'd
IF FORCED LANDING ANTICIPATED
APPROACH
— MIN RAT SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .140 KT
At a suitable altitude (not below 3000 feet AGL), configure the
aircraft for landing (CONF 1; L/G DOWN)
— LAND RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT
EMER GEN is lost at slats' extension. The aircraft is supplied by batteries only.
— MAX SPEED for GRAVITY EXTENSION . . . . . . . . . . . . . . . .250 KT
— L/G GRAVTY EXTN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
Disregard "USE MAN PITCH TRIM" on the PFD, because the stabilizer is frozen in the
position it was at, when the windmilling was insufficient to provide hydraulic power.
When L/G downlocked
— L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
— APPROACH SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . 190 KT
Adjust the speed to the Vapp given above. However, to reach the landing field/runway,
the approach speed may be adjusted up to 250 knots (max speed with landing gear
extended)
— GND SPLR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARM
— MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1000 PSI
AT 1000 FEET AGL
— CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"
AT 200 FEET
— BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"
AT TOUCHDOWN
— ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— BRAKES ON ACCU ONLY
AFTER LANDING
When the aircraft has stopped :
—
—
—
—
—
PARKING BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE
BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING
If not, switch on the transmitter
VI6 ALL
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A340-600
EMERGENCY PROCEDURES
REV 25
SEQ 205
1.19
ENG ALL ENG FLAMEOUT-NO FUEL REMAINING Cont'd
IF DITCHING ANTICIPATED
APPROACH
— MIN RAT SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .140 KT
At a suitable altitude (not below 3000 feet AGL), configure the
aircraft for ditching (CONF 1, L/G UP)
— LAND RECOVERY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT
EMER GEN is lost at slats' extension. The aircraft is supplied by batteries only.
— L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK UP
— APPROACH SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . .190 KT
AT 1000 FEET AGL
— CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"
— DITCHING pushbutton . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
In case of strong crosswind, ditch face to the wind.
In the absence of strong crosswind, prefer ditching parallel to the swell. Touchdown
with approximately 11 degrees of pitch and minimum aircraft vertical speed.
R
R
R
R
AT 200 FEET
— BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"
AT TOUCHDOWN
— ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
AFTER DITCHING
— ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
— EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE
— BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING
If not, switch on the transmitter
VI6 ALL
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1.20
REV 24
EMERGENCY PROCEDURES
A340-600
SEQ 001
TWO ENGINE INOP LANDING
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*
VIRGIN ATLANTIC AIRWAYS REVISION 10 / 01 May 2005
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A340-600
EMERGENCY PROCEDURES
REV 25
SEQ 100
1.21
DITCHING
This procdure applies when engines are running. If engines are not running, refer to the QRH
"ALL ENGINE FLAME OUT" (with or without fuel remaining) procedures, which has been
amended to include the ditching procedure, when the engines are running.
PREPARATION
— ATC/TRANSPONDER (if available) . . . . . . . . . . .NOTIFY/AS RQRD
Notify ATC of the nature of the emergency encountered, and state intentions. If not in contact
with ATC, select transponder code A7700, or transmit the distress message on :
(VHF) 121.5 MHZ or (HF) 2182 KHZ or 8364 KHZ.
— CABIN and COCKPIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PREPARE
— Loose equipment secured.
— Survival equipment prepared.
— Belts and shoulder harnesses locked.
— JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— GPWS SYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— GPWS TERR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
R
— SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— LDG ELEV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SELECT 00
— BARO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SET
Omit the normal approach and landing checklist.
— CREW MASKS/OXY SUPPLY (below FL 100) . . . . . . . . . . . . . . .OFF
APPROACH
— L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UP
— SLATS and FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAX AVAIL
— JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
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A340-600
EMERGENCY PROCEDURES
REV 25
SEQ 100
1.22
DITCHING (Cont'd)
AT 1000 FEET AGL
— CAB PRESS MODE SEL . . . . . . . . . . . . . . . . . . .CHECK AUTO
— BLEED (ENGs and APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"
— DITCHING pushbutton . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
In case of strong crosswind, ditch face to the wind.
In the absence of strong crosswind, prefer ditching parallel to the swell. Touchdown
with approximately 11 degrees of pitch and minimum aircraft vertical speed.
AT 200 FEET
— BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"
AT TOUCHDOWN
— ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— APU MASTER SW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
AFTER DITCHING
— ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
— FIRE pushbutton (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . .PUSH
— AGENTS (ENG and APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DISCH
— EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE
— BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING
If not, switch on the transmitter
VI6 ALL
VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006
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A340-600
EMERGENCY PROCEDURES
REV 25
SEQ 100
1.23
FORCED LANDING
This procedure applies when engines are running. If engines are not running, refer to the
QRH "ALL ENG FLAME OUT" (with or without fuel remaining) procedure, which has been
amended to include the forced landing procedure, when the engines are not running.
PREPARATION
— ATC/TRANSPONDER (if available) . . . . . . . . . . .NOTIFY/AS RQRD
Notify ATC of the nature of the emergency encountered, and state intentions. If not in contact
with ATC, select transponder code A7700, or transmit the distress message on :
(VHF) 121.5 MHZ or (HF) 2182 KHZ or 8364 KHZ.
— CABIN and COCKPIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PREPARE
— Loose equipment secured.
— Survival equipment prepared.
— Belts and shoulder harnesses locked.
— JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— GPWS SYS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— GPWS TERR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
R
— SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— LDG ELEV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SELECT 00
— BARO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SET
Omit normal approach and landing checklist.
— CREW MASKS/OXY SUPPLY (below FL 100) . . . . . . . . . . . . . . .OFF
APPROACH
— RAM AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
— SLATS and FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAX AVAIL
— GND SPLR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ARM
— JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1000 PSI
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A340-600
EMERGENCY PROCEDURES
REV 24
SEQ 200
1.24
FORCED LANDING (Cont'd)
AT 1000 FEET AGL
— CABIN (CM2) . . . . ."CABIN CREW TO EMERGENCY STATIONS"
AT
200 FEET
— BRACE
FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . ."BRACE BRACE"
AT TOUCHDOWN
— ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— APU MASTER SW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— BRAKES ON ACCU ONLY
AFTER LANDING
When the aircraft has stopped :
—
—
—
—
—
—
—
PARKING BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
FIRE pushbutton (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . .PUSH
AGENTS (ENG and APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DISCH
EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE
BAT 1+2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK EMITTING
If not, switch on the transmitter
VI6 ALL
VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006
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A340-600
EMERGENCY PROCEDURES
REV 24
1.25
SEQ 001
EMER DESCENT
IMMEDIATE ACTIONS
- CREW OXY MASKS . . . . . . . . . . . . . . . . . . . . . . . . . .ON
BOTH
Set the oxygen diluter selector to the N position.
NOTE:
With the oxygen diluter selector left at 100%, oxygen quantity
may not be sufficient for the entire emergency descent profile.
The recommendation is to descend with the A/P engaged :
• Turn the ALT selector knob and pull.
• Turn the HDG selector knob and pull.
• Adjust target SPD/MACH.
- THRUST . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLE
PF
• If autothrust is engaged, check IDLE on the UPPER ECAM.
• If not engaged, retard the thrust levers.
- SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FULL
PF
WHEN DESCENT ESTABLISHED
EMER DESCENT FL 100, or MEA (whichever is higher)
- SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX/APPROPRIATE
CAUTION
Descend at the maximum appropriate speed. If structural damage is
suspected, use the flight controls with care and reduce speed as appropriate.
Landing gear may be extended below 21,000 feet. Speed must be reduced to VLO.
- SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
-- ENG
. . . .IGN
ATC .START
. . . . . . . SEL
. . . . ....... .. .. .. .. .. .. .. .. .. ......... .. .. .. .. .. .. .. .. .. ............. .. ..NOTIFY
IF CAB ALT > 14,000 feet:
- PAX OXY MASKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAN ON
. Confirm passenger oxygen masks released.
Note:
VI6 ALL
Notify the cabin crew, when a safe flight level has been reached
and oxygen mask use can be terminated.
VIRGIN ATLANTIC AIRWAYS REVISION 10 / 01 May 2005
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EMERGENCY PROCEDURES
A340-600
REV 00
SEQ VAA
1.26
CABIN FIXED OXYGEN SYSTEM
CABIN OXYGEN ENVELOPE
FLIGHT
LEVEL
400
290
300
250
200
100
0
0 1 2
3 4
5 6 7
8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23
TIME (MIN)
Any emergency descent profile with passengers supplied by chemical oxygen generators must be
executed below boundary given in the figure.
NOTE:
VI6 ALL
30 minutes now allowed (JAR's) at FL 140 prior to descent to FL 100.
VIRGIN ATLANTIC AIRWAYS REVISION 10 / 01 May 2005
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A340-600
REV 25
ABNORMAL PROCEDURES
2.00
SEQ 402
CONTENTS
R
R
R
R
R
AUTO FLT
 LOSS OF FMS DATA IN DESCENT/APPROACH
(SEVERE RESET) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• MCDU FAILURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.00B
2.01
EQUIPMENT
• COCKPIT DOOR FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.01
F/CTL
• RUDDER JAM/RUDDER PEDAL JAM . . . . . . . . . . . . . . . . . .
• RUDDER TRIM RUNAWAY . . . . . . . . . . . . . . . . . . . . . . . . . .
• LDG WITH FLAPS/SLATS JAMMED . . . . . . . . . . . . . . . . . .
• NO FLAPS NO SLATS LANDING . . . . . . . . . . . . . . . . . . . . .
• LOW ENERGY WARNING . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.02
2.03
2.05
2.06A
2.06
FUEL
• GRVTY FUEL FEEDING . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• WING TK IMBALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FUEL LEAK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FUEL IMBALANCE PROCEDURES TANKS 1 & 2 AND
TANKS 3 & 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FUEL JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FUEL LOSS REDUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . .
• TRIM TANK FUEL UNUSABLE . . . . . . . . . . . . . . . . . . . . . . .
• FUEL LO TEMP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.08B
2.09
2.09
2.10
2.10A
ICE AND RAIN PROTECTION
• DOUBLE STAT (AOA) HEAT FAILURE . . . . . . . . . . . . . . . . .
2.11
INDICATING/RECORDING
• DISPLAY UNIT FAILURE .
• ECAM SINGLE DISPLAY .
• TAILSTRIKE . . . . . . . . . . .
• DISPLAY DISCREPANCY .
2.11
2.11A
2.11A
2.12
..
..
..
..
. .. .. . .. . .. .. . .. .. . .. .. .
.. .. .. .. .. .. .. .. .. .. .. ..
. .. .. . .. .. . .. . .. . .. . .. ..
.. .. .. . .. . .. . .. .. . .. . .. .
LANDING GEAR
• L/G GRAVITY EXTENSION . . . . . . . . . . .
• LDG WITH ABNORMAL CENTER L/G . . .
• LDG WITH ABNORMAL NOSE/MAIN L/G .
• RESIDUAL BRAKING PROC. . . . . . . . . . .
..
..
..
..
..
..
..
..
.. .. ..
.. .. ..
.. .. ..
. .. . ..
..
..
..
..
..
..
..
..
NAV
• FM/GPS POS DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . .
• ADR 1+2+3 FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• ADR DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• ADR CHECK PROC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• UNRELIABLE SPEED INDICATION . . . . . . . . . . . . . . . . . . .
• IR ALIGNMENT IN ATT MOD . . . . . . . . . . . . . . . . . . . . . . . .
2.07
2.07
2.08
2.13
2.14
2.15
2.17
2.18
2.19
2.20
2.20A
2.21
2.24
VI6 MSN 0371-0615
VIRGIN ATLANTIC AIRWAYS REVISION 11 / 15 August 2005
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MSN 0622-0765
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A340-600
ABNORMAL PROCEDURES
REV 25
2.00
SEQ 505
CONTENTS
R
R
R
R
R
AUTO FLT
• LOSS OF FMS DATA IN DESCENT/APPROACH
(SEVERE RESET) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• MCDU FAILURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.00B
2.01
EQUIPMENT
• COCKPIT DOOR FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.01
F/CTL
• RUDDER JAM/RUDDER PEDAL JAM . . . . . . . . . . . . . . . . . .
• RUDDER TRIM RUNAWAY . . . . . . . . . . . . . . . . . . . . . . . . . .
• LDG WITH FLAPS/SLATS JAMMED . . . . . . . . . . . . . . . . . .
• NO FLAPS NO SLATS LANDING . . . . . . . . . . . . . . . . . . . . .
• LOW ENERGY WARNING . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.02
2.03
2.05
2.06A
2.06
FUEL
• GRVTY FUEL FEEDING . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• WING TK IMBALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FUEL LEAK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FUEL IMBALANCE PROCEDURES TANKS 1 & 2 AND
TANKS 3 & 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FUEL JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FUEL LOSS REDUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . .
• TRIM TANK FUEL UNUSABLE . . . . . . . . . . . . . . . . . . . . . . .
• FUEL LO TEMP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.08B
2.09
2.09
2.10
2.10A
ICE AND RAIN PROTECTION
• DOUBLE STAT (AOA) HEAT FAILURE . . . . . . . . . . . . . . . . .
2.11
INDICATING/RECORDING
• DISPLAY UNIT FAILURE .
• ECAM SINGLE DISPLAY .
• TAILSTRIKE . . . . . . . . . . .
• DISPLAY DISCREPANCY .
2.11
2.11A
2.11A
2.12
..
..
..
..
. .. . .. .. . .. .. . .. .. . .. .. .
.. .. .. .. .. .. .. .. .. .. .. ..
. .. .. . .. .. . .. . .. . .. . .. ..
.. .. .. . .. . .. . .. .. . .. . .. .
2.07
2.07
2.08
LANDING GEAR
• L/G GRAVITY EXTENSION . . . . . . . . . . . . . . . . . . . . . . . . .
• LDG WITH ABNORMAL CENTER L/G . . . . . . . . . . . . . . . . .
2.13
2.14
NAV
• FM/GPS POS DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . .
• ADR 1+2+3 FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• ADR DISAGREE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• ADR CHECK PROC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• UNRELIABLE SPEED INDICATION . . . . . . . . . . . . . . . . . . .
• IR ALIGNMENT IN ATT MOD . . . . . . . . . . . . . . . . . . . . . . . .
2.18
2.19
2.20
2.20A
2.21
2.24
VI6 MSN 0622-0765
VIRGIN ATLANTIC AIRWAYS REVISION 11 / 15 August 2005
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MSN 0371-0615
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A340-600
R
ABNORMAL PROCEDURES
2.00A
REV 25
SEQ 100
POWER PLANT
• ENG RELIGHT IN FLIGHT . . . . . . . . . . . . . . . . . . . . . . . . . .
• ENG STALL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• HIGH ENGINE VIBRATION . . . . . . . . . . . . . . . . . . . . . . . . . .
2.26
2.27
2.28
• ENG TAILPIPE FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2.28
MISCELLANEOUS
• OVERWEIGHT LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . .
• COCKPIT WINDSHIELD/WINDOW CRACKED . . . . . . . . . . .
• COCKPIT WINDSHIELD/WINDOW ARCING . . . . . . . . . . . . .
• VOLCANIC ASH ENCOUNTER . . . . . . . . . . . . . . . . . . . . . . .
• BOMB ON BOARD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• RESET OF COMPUTERS . . . . . . . . . . . . . . . . . . . . . . . . . . .
• ECAM ADVISORY CONDITIONS . . . . . . . . . . . . . . . . . . . . .
• VAPP DETERMINATION . . . . . . . . . . . . . . . . . . . . . . . . . . .
• LDG CONF/APP SPD/LDG DIST FOLLOWING FAILURES. .
2.29
2.30
2.30
2.30
2.31
2.35
2.38
2.40
2.41
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A340-600
ABNORMAL PROCEDURES
REV 22
SEQ 102
2.01
MCDU 1 (2) (3) FAILURE
— BRT KNOB (on affected MCDU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
MCDU 3 automatically replaces MCDU 1 or 2.
COCKPIT DOOR FAULT
This procedure should be applied, if the Cockpit Door Locking System (CDLS) fails. This Failure
is indicated when the FAULT light on the center pedestal's CKPT DOOR panel comes on.
— CKPT DOOR CONT PANEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
This panel is located on the overhead panel. It is used to identify the faulty CDLS item, and to
verify the status of the pressure sensors and the three electrical latches (referred to as strikes).
If two or more electrical latches (strikes) are faulty :
The cockpit door is not intrusion-proof.
If two pressure sensors are faulty :
Automatic latch release is unavailable, in case of cockpit decompression.
If no LED on the CKPT DOOR CONT panel is on :
The CDLS control unit is faulty; therefore, the cockpit door might unlock automatically. If
it does not, consider using the mechanical override system to unlock the door.
NOTE : In case of a DC BUS 2 fault, no FAULT indication appears on the center pedestal's CKPT
DOOR panel. The CDLS is not electrically-supplied, and is inoperative.
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A340-600
ABNORMAL PROCEDURES
REV 23
SEQ 102
2.02
F / CTL RUDDER JAM/RUDDER PEDAL JAM
Rudder jam :
In case of a rudder jam, the rudder pedals are not jammed.
•
If theRUDDER
rudder is jameed
the 0° warning
position :will automatically be triggered. Refer to this
The
FAULT inECAM
procedure.
If the rudder is jammed in a position other than 0° :
Unusual pedal movement or position, which corresponds to the computed rudder trim
value, may indicate a rudder jam.
AP can be used. However, automatic landing is not authorized.
When engaged, the autopilot introduces rudder trim, and so, pedal deflection.
When the rudder trim reaches 25°, the indication is dashed on the RUDDER TRIM panel.
At autopilot disengagement, this pedal deflection remains.
Use the ECAM F/CTL page for a visual check of the rudder position.
•
BEFORE FINAL APPROACH
— AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISENGAGE
— RUDDER TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESET
Rudder pedal jam :
The rudder operates normally, and automatic landing is recommended.
If an autoland is performed, do not apply the following approach procedure.
FOR APPROACH
— AVOID LANDING WITH CROSSWIND from the side where the rudder is
deflected.
— FOR LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE FLAP 2
— GPWS FLAP MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
— SPEED and TRAJECTORY . . . . . . . . . . . . . . . . . . STABILIZE ASAP
— LDG DIST PROC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY
R
R
Multiply the landing distance by 1.1 on dry runway or by 1.15 on wet or contaminated
runway.
ON GROUND
— DIFFERENTIAL BRAKING . . . . . . . . . . . . . . . . . . . . . . . USE ASAP
Do not use asymmetrical thrust reverse.
Use nosewheel steering handle below 100 knots.
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A340-600
ABNORMAL PROCEDURES
REV 19
SEQ 100
2.03
F / CTL RUDDER TRIM RUNAWAY
— LATERAL CONTROL . . . . . . . . . . . . . . . . . . . . USE TO LEVEL WINGS
— RUDDER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CENTRALIZE
Check the rudder position on the ECAM F/CTL page.
Note : This failure will be seen mainly as uncommanded roll (induced by yaw). In most
conditions, the aircraft will self stabilize in a steady heading sideslip.
For continued flight, either maintain rudder central or leave the aircraft in a steady
stabilized heading sideslip, but ensure that all changes between rudder centralized
and steady heading sideslip are made smoothly. As speed is reduced, the Rudder
Travel Limit may gradually open to allow more rudder to be applied by the trim runaway.
R
— FOR LDG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE NORMAL CONF
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A340-600
ABNORMAL PROCEDURES
REV 13
SEQ 210
2.04
LEFT INTENTIONALLY BLANK
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A340-600
ABNORMAL PROCEDURES
REV 00
SEQ VAA
2.08B
FUEL IMBALANCE PROCEDURES TANKS 1 & 2 AND TANKS 3 & 4
Note: DO NOT BALANCE INNER TANKS (1 and 2) + (3 and 4) AT THE
SAME TIME.
If significant imbalance between Inner Tanks 1 and 2:
— X-FEED 1 + 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— STBY 1 (2) (lighter side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— MAIN 1 (2) (lighter side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
When tanks are balanced, recover normal configuration by,
— MAIN and STBY pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— X-FEEDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CLOSE
If significant imbalance between Inner Tanks 3 and 4:
— X-FEED 3 + 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— STBY 3 (4) (lighter side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
— MAIN 3 (4) (lighter side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
When tanks are balanced, recover normal configuration by,
— MAIN and STBY pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— X-FEEDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CLOSE
Note: Do not exceed 2500 kg between inner tanks 1 and 4, 3000 kg between
inner tanks 2 and 3, in order to avoid the FUEL WING TK IMBALANCE
ECAM caution to be triggered.
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R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
R
ABNORMAL PROCEDURES
REV 25
2.09
SEQ 100
FUEL LOSS REDUCTION
Apply this procedure only if suggested by the FUEL LEAK procedure, and if
the flight crew needs to minimize the fuel loss. It covers two type of leak :
- A leak from wing : a manual Trim tank transfer (via the Center tank) and/or
manual
tank transfer
canautomatic
be done, to
symmetrically
transfer
the
fuel to allCenter
inner tanks,
and avoid
transfer
to only the
least full
inner tank.
- A leak from the Center tank, or the Trim tank : a manual Trim and/or
Center tank transfer to the inner tanks can be done to save some Trim or
Center tank fuel.
If Center Tank or Trim Tank not empty :
— CTR TO INR L + R PUMPS . . . . . . . . . . . . . . . . . . . . . . . , . . . . . .ON
— CTR TO INR XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN
— T TK FEED (if not empty) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO
— T TK XFR (if not empty) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FWD
When Trim Tank empty :
— T TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
— T TK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ISOL
When Center Tank empty :
— CTR TO INR XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AUTO
FUEL JETTISON
WARNING
If the jettison procedure is applied following the "FUEL LEAK" or "ENG FAIL"
with tank damage procedure, the flight crew must comply with the following
requirements:
— If a fuel leak is present, and weight reduction is essential for landing, once
close to the landing airfield, adopt the following procedure for fuel jettison.
It is possible to jettison in any convenient configuration and at any speed.
When practicable, the height should be sufficient to avoid contamination on
the ground (5,000 feet is considered adequate).
Do not jettison in a thunderstorm.
When jettisoning is performed, avoid flying into the jettisoned flow (which is
descending at about 500 ft/min).
Average weight reduction (by jettison only) is 1600 kg/min.
On the MCDU:
— FUEL PRED key . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SELECT
— JET GW . . . . . . . . . . . . . . . . . . . . . . . . . . . .ENTER THE FINAL GW
On the OVERHEAD panel:
— JETTISON ARM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
— JETTISON ACTIVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
CAUTION: During jettison operation, monitor the CG. If either the forward
or
aft takeoff
and in
landing
limit is reached,
jettison.
When
jettisoning
clean configuration,
dostop
not use
speedbrakes.
When JETTISON is completed, or to manually stop the JETTISON
operation:
JETTISON ACTIVE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
JETTISON ARM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Notes: Jettison operation is automatically stopped when:- Fuel WING TK LO LVL warning threshold is reached.
- Actual GW reaches the value inserted in the MCDU.
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ABNORMAL PROCEDURES
REV 25
SEQ 105
2.10
TRIM TANK FUEL UNUSABLE
T TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FWD
T TK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN
If TRIM TANK FUEL still unusable
— OUTR TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
— CTR TO INR L and R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
— CTR AFT XFR L and R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
MAXIMUM FLIGHT TIME . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 HOURS
After 4 hours, depending on the fuel distribution, the aft CG limit may be
reached.
FOR LANDING
If CG > aft CG limit shown below :
R
R
— APPR SPD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VLS + 10 KT
— LDG DIST PROC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY
Multiply the landing distance by 1.20 on dry runway, or 1.20 on wet runway,
or 1.20 on contaminated runway.
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ABNORMAL PROCEDURES
REV 00
SEQ VAA
2.10A
FUEL LO TEMP
NOTE:
Before carrying out this drill refer to the Tech Log to check
on the fuel uplifted and its freezing point. (NB: JET A (F
point -40°C) is normally only uplifted in USA.
Any fuel temperature below - 40°C
On ground, before takeoff:
IF JET A FUEL:
— DELAY T.O
Do not takeoff, until temperatures are within limits.
In flight:
If outer tank temp <-40° C (automatic recall at -47°C)
IF JET A FUEL
MAX SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 305 KT
— OUTR TK XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN
If trim tank temp <-40° C (automatic recall at -47°C)
IF JET
FUEL
—
T TKAXFR
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FWD
Fuel consumption increases by approximately 2%.
Note: If the trim tank pumps are failed, this part of the procedure will
be replaced by:
WHEN SPD >270KT AND NOT IN CLIMB:
—
T TK XFR . . . . . . FWD
If inner tank temp <-40° C (automatic recall at -47°C)
IF JET A FUEL
— CTR TO INR XFR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN
IF NECESSARY:
— TAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE
Consider descending to a lower altitude and/or increasing Mach to
increase
TAT.
Note: 1. The
caution
is automatically recalled, when:
Any tank temperature is below - 47°C. In this case, " IF JET A" is not
displayed in the procedure.
2. If a fuel type, other than Jet A is used, see 3.01.28 page 1 for the
appropriate limits, and apply the procedure according to those limits.
STATUS
APPR PROC
AT SLATS EXTENSION:
— T TK XFR . . . . . . . . . . . . AUTO
Manual trim tank transfer must be stopped at slats'
extension, to avoid CG changes during approach.
If both trim tank transfer pumps have failed:
LVL OFF FOR MAN FWD XFR
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ABNORMAL PROCEDURES
REV 25
SEQ 100
2.11A
ECAM SINGLE DISPLAY
Only the EWD is available. No SD on the other DUs.
To call a SYS page:
— PRESS AND MAINTAIN the SYS page key on the ECP
OVERFLOW ON THE STATUS page:
— PRESS AND MAINTAIN the SYS key on the ECP
The first page of the STATUS is displayed.
— RELEASE IT, THEN PRESS IT AGAIN WITHIN 2 SECONDS
The second page of the STATUS is displayed.
— CONTINUE UNTIL THE OVERFLOW ARROW DISAPPEARS
When the STS key is released for more than 2 seconds, the EWD is
displayed again.
TAILSTRIKE
When a tail strike is experienced apply the following procedure
LAND ASAP
— MAX FL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 100 or MSA
500 feet/minute should be targeted for the climb, to minimise pressure
changes, for passenger and crew comfort. Similarly, the rate of descent
must be limited to about 1000 feet/minute, except for the final approach,
that must be performed normally.
Notify the ATC of the aircraft's rate of climb.
— RAM AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
— PACK 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
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A340-600
ABNORMAL PROCEDURES
REV 25
SEQ 100
2.15
LDG WITH ABNORMAL NOSE/MAIN L/G
PREPARATION
— CABIN CREW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY
— ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY
— JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONSIDER
If NOSE L/G abnormal
— CG location (if possible) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AFT
. 10 passengers from front to rear moves the CG roughly 2% aft.
If one MAIN L/G abnormal
— FUEL IMBALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONSIDER
. Open all the fuel crossfeed valves, and switch off the pumps on the side with
landing gear normally extended.
— OXYGEN CREW SUPPLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
— SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
— CABIN and COCKPIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PREPARE
R
. Loose equipment secured.
. Survival equipment prepared.
. Belts and shoulder harness locked.
APPROACH
— GPWS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
— L / G GRVTY EXTN . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK DOWN
—
—
—
—
—
—
—
L/G LEVER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK DOWN
AUTOBRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT ARM
EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
COMMERCIAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
CABIN REPORT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OBTAIN
JETTISON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
T TANK FEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ISOL
If one MAIN L/G abnormal
— GROUND SPOILERS . . . . . . . . . . . . . . . . . . . . . . . . . .DO NOT ARM
APPROACH
— RAM AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
— BRACE FOR IMPACT . . . . . . . . . . . . . . . . . . . . . . . . . . ORDER
cont'd
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ABNORMAL PROCEDURES
REV 21
SEQ 100
2.16
LDG WITH ABNORMAL NOSE/MAIN L/G (Cont'd)
FLARE, TOUCHDOWN, AND ROLLOUT
Engines should be shut down sufficiently early to ensure fuel is shut off before the
nacelles impact, but sufficiently late to ensure adequate hydraulic supplies for the flight
controls. Hydraulic pressure for flight controls remains available for 30 seconds after
the shut down of engines 1 and 4.
If NOSE L/G abnormal
— REVERSE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT USE
— NOSE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN UP
After touchdown, keep the nose off the runway by using the elevator.
Then, lower the nose onto the runway before elevator control is lost.
— BRAKES (compatible with elevator efficiency) . . . . . . . . . APPLY
— ENG MASTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Shut down the engines before nose impact.
If one MAIN L/G abnormal
— REVERSE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT USE
— ENG MASTERS (in sequence) . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
After main gear touchdown, shut down the outboard engines first, then the
inboard engines (failure side first) before nacelle touchdown.
— FAILURE SIDE WING . . . . . . . . . . . . . . . . . . . . . . MAINTAIN UP
Use roll control, as necessary, to keep the unsupported wing up as long as
possible.
— DIRECTIONAL CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN
R
Use rudder and brakes (maximum 1000 psi) to maintain runway axis as long
as possible.
WHEN A/C STOPPED
— ENG (all) and APU FIRE pushbutton . . . . . . . . . . . . . . . . . . . . . . PUSH
Pressing the ENG FIRE pushbutton shuts off the related hydraulic pressure
within a short time.
— ENG (all) and APU AGENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCH
R
— EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE
Announce : "PASSENGER EVACUATION" over the PA. All emergency and
passenger doors may be used to evacuate the aircraft. If one main landing
gear is not extended, the aircraft will rest on the nose gear and outer engine(s).
VIRGIN ATLANTIC AIRWAYS REVISION 03 / 22 May 2003
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A340-600
ABNORMAL PROCEDURES
REV 21
SEQ 050
2.27
ENG 1(2)(3)(4) STALL
A stall may be indicated by varying degrees of abnormal engine noises,
accompanied by flame from the engine exhaust and possibly from engine inlet in
severe cases, fluctuating parameters, sliggish or no thrust lever response, high EGT
and/or a rapid EGT rise when thrust lever is advanced. Engine stalls must be
reported for maintenance action.
Stall is detected by the FADEC :
If on ground :
— THR LEVER (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
— ENG MASTER (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . OFF
If the crew detects a stall before the ECAM activation :
The following procedure may be applied :
— THR LEVER (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
— ENG PARAMETERS (affected engine) . . . . . . . . . . . . . . . . . . . . . CHECK
If abnormal parameters :
— ENG MASTER (affected engine) . . . . . . . . . . . . . . . . . . . . OFF
ENG 1(2)(3)(4)
SHUT DOWN
Apply ENG SHUT DOWN procedure.
Engine restart at crew discretion.
If normal parameters :
— ENG A ICE (affected engine) . . . . . . . . . . . . . . . . . . . . . . . ON
— WING A ICE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Operation of ENG and WING A ICE will increase the stall margin but EGT
will increase accordingly.
— THR LEVER . . . . . . . . . . . . . . . . . . . . . . . . . . SLOWLY ADVANCE
if stall does not reoccur :
— Continue engine operation
cont'd
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ABNORMAL PROCEDURES
REV 23
SEQ 050
2.28
HIGH ENGINE VIBRATION
R
R
The ECAM's VIB advisory mainly serves as a guideline to induce the crew to closely
monitor and crosscheck engine parameters.
VIB detection alone does not require engine shutdown.
NOTE :
High engine vibrations may be accompanied by cockpit and cabin
smoke, and /or burning smells. This may be due only to compressor
blade tip contact with associated abradable seals.
High N1 vibrations are generally accompanied by perceivable airframe
vibrations.
High N2/N3 vibrations can exist without perceivable airframe vibrations.
IF NO ICING CONDITIONS EXIST :
ENG PARAMETERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Check engine parameters and especially EGT ; crosscheck with the other
engines.
Report in maintenance log.
If rapid increase above the advisory :
— THRUST LEVER (affected engine) . . . . . . . . . . . . . . . . . . . . RETARD
Flight conditions permitting reduce N1 to maintain the vibration level below
the advisory threshold.
NOTE : If the VIB indication does not decrease following thrust reduction,
this may indicate other engine problems. Apply the applicable
procedure.
IF NO ICING CONDITIONS EXIST :
An increase of N1 vibration in icing conditions, with or without engine anti-ice,
may be due to fan blades and /or spinner icing.
— A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
— ENGINE ANTI ICE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
If still OFF, ENG ANTI ICE should be switched ON at idle fan speed, one engine
after the other, at an approximate interval of 30 seconds.
— THRUST (one engine at a time). . . . . . . . . . . . . . . . . . . . . . . . INCREASE
Increase thrust with the power setting compatible with the flight phase. The VIB
level will return to normal after ice shedding, despite a light increase during
acceleration.
Resume normal operation.
NOTE : If possible, shut down the engine after landing, for taxiing, when
vibrations above the advisory level have been experienced during
the flight.
VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006
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ABNORMAL PROCEDURES
REV 00
SEQ VAA
2.28A
ENG TAILPIPE FIRE
Internal engine fire may be encountered during engine start, or engine shutdown.
It may be seen by the ground crew, or the EGT may fail to decrease after the MASTER
switch is turned off.
CAUTION
External fire agents can cause severe corrosive damage and should,
therefore, only be considered after having applied the following procedure :
— ENG MASTER (affected) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Note : Do not press the engine fire pushbutton, since this would cut off the
FADEC power supply, which would prevent motoring sequence.
— AIR BLEED PRESS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ESTABLISH
. Select the APU, or the opposite ENG BLEED, to motor the engine.
. If APU BLEED is not available, and the other engine is shut down, connect
external pneumatic power (if readily available).
— BEACON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
When N3 < 30 %
— ENG START SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CRANK
— MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
When burning has stopped :
— MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
— ENG START SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
R
Maintenance action is due.
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NORMAL PROCEDURES
SEQ 001
REV 11
3.00
CONTENTS

SAFETY EXTERIOR INSPECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.01
• PRELIMINARY COCKPIT PREPARATION . . . . . . . . . . . . . . . . . . . . . . . . . .3.01
• AFTER LANDING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3.02
• PARKING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3.02
•
SECURING THE AIRCRAFT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3.02
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NORMAL PROCEDURES
A340-600
REV 24
SEQ 200
3.01
SAFETY EXTERIOR INSPECTION
SECURITY CHECK
FLIGHT DECK & FLIGHT CREW REST AREA . . . . . . . . . . . . . . PERFORM
CM1
CM2
CM2
NOSE WHEEL CHOCK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN PLACE
L/G DOORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK POS.
APU AREA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
PRELIMINARY COCKPIT PREP
CM1
ENTER FLIGHT NUMBER IN INIT PAGE 'A'
COMPLETE AND SEND LOAD SHEET PAGE 1
INCLUDING RTOW
(IF ACARS STBY, PERFORM IRS ALIGNMENT
FOR SATELLITE COMMUNICATION)
CM2
EMER EQPTS . . . . . . . . . . . . . . . . . . .. . . . . . . . . . .CHECK
ENG panel . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . .CHECK
L/G lever . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
WIPERS . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
BAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
EXT PWR . . . . . . . . . . . . . . . . . . . . . . . . . .ON
BAT . . . . . . . . . . . . . . . . . . . . . . . .CHECK/.AUTO
APU FIRE . . . . . . . . . . . . . . . . . . .CHECK/TEST
APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .START
EXT PWR . . . . . .. . . . . . . . . . . . . . . . . . AS RQRD
COCKPIT LT . . . . . . . . . . . . . . . . . . . . .AS RQRD
PARKING BRK .. . . . . . . . . . . . . . . . . . . . . . . . . ON
ACCU/BRAKE PRESS .. . . . . . . . . . . . . . . . . . . . . .CHECK
FLAPS . . . . . . . . . . . . . . . . . . . . . . CHECK POSITION
SPEEDBRAKE .. . . . . . . . . . . . . . . .CHECK RET
PROBES/WINDOW HEAT . . . . . . . . . . . . . . .AUTO
APU BLEED . . . . . . . . . . .. . . . . . . . . . . . . .ON
AIR COND panel . . . . . .. . . . . . . . . . . . . . . .SET
ELEC panel . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
VENT panel . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
ECAM RECALL .. . . . . . . . . . . . . . . . . . . . . DEPRESS
ECAM HYD QTY, ENG OIL QTY . . . . . . . . . CHECK
EXT WALK ROUND . . . . . . . . . . . . .PERFORM
PNF
VIRGIN ATLANTIC AIRWAYS REVISION 11 / 15 August 2005
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REV 00
SEQ VAA
3.02
AFTER LANDING
PNF
PF
GRND SPLRS . . . . . . . . . . . . . . . . . . . . . . . . . . .DISARM RADAR . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF/STBY
(signal for PNF to commence after landing items) FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RETRACT
NOSE LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TAXI TCAS (as installed) . . . . . . . . . . . . . . . . . . . . . . .STBY
ENG START sel . . . . . . . . . . . . . . . . . . . . . . . . . .NORM
EXT LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . .AS RQRD
ANTI ICE . . . . . . . . . . . . . . . . . . . . . . . . . . . AS RQRD
APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .START
BRAKES TEMP . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
AFTER LDG C/L
PARKING
CM 1
CM 2
PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . .ON
APU BLEED . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
ENG MASTER 1, 2, 3, 4 . . . . . . . . . . . . . . . . . . . .OFF
SLIDE DISARMED . . . . . . . . . . . . . . . . . . . . . . .CHECK
ELAPSED TIME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .STOP
BEACON LT . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
EXT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AS RQRD
SEAT BELTS . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
GROUND CONTACT . . . . . . . . . . . . . . . . . . . ESTABLISH
PARKING BRK . . . . . . . . . . . . . . . . . . . . . . .AS RQRD
PARKING C/L
FUEL PUMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
STATUS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
IRU DRIFT RATE . . . . . . . . . . . . . . . . . . . . . . . .CHECK
SECURING THE A/C
CM 1
CM 2
ADIRS (1 + 2 + 3) . . . . . . . . . . . . . . . . . . . . . . . .OFF FMGS POSTFLIGHT REPORT . . . . . . . . . . . PRINT
CMS POST FLT REPORT . . . . . . . . . . . . . . . AS RQRD OXY CREW SUPPLY . . . . . . . . . . . . . . . . . . . . . .OFF
DUs . . . . . . . . . . . . . . . . . . . . . . . . . . . .DIM or OFF EXT LT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
TECH LOG . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETED APU BLEED . . . . . . . . . . . . . . . . . . . . . . . . AS RQRD
EXT PWR . . . . . . . . . . . . . . . . . . . . . . . . . . AS RQRD
APU MASTER SW . . . . . . . . . . . . . . . . . . . . AS RQRD
EMER EXIT LT . . . . . . . . . . . . . . . . . .. . . . . . . . .OFF
NO SMOKING . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
BAT 1 + 2 + APU . . . . . . . . . . . . . . . . . . . . . .AS REQD
DU's . . . . . . . . . . . . . . . . . . . . . . . . . . . DIM or OFF
SECURING THE A/C C/L
VIRGIN ATLANTIC AIRWAYS REVISION 10 / 01 May 2005
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IN FLIGHT PERFORMANCE
REV 10
SEQ 001
4.00
CONTENTS

•
•
•
•
SPEEDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF 3 . . . . . . .
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF FULL . . . .
AUTOLAND LANDING DISTANCE WITH AUTOBRAKE . . . . . . . . .
ENG OUT
MAX ALTITUDE (ONE or TWO or THREE ENGINES OUT) . . . .
GROSS FLIGHT PATH DESCENT AT GREEN DOT SPEED . .
LONG RANGE CRUISE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
IN CRUISE QUICK CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• ALL ENGINES
CLIMB CEILING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
MAX/OPT ALTITUDES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
IN CRUISE QUICK CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . .
COST INDEX . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
DESCENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4.01
4.02
4.03
4.04
DIVERSION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FLIGHT WITHOUT CAB PRESS . . . . . . . . . . . . . . . . . . . . . . . . . .
• GROUND DISTANCE-AIR DISTANCE CONVERSION . . . . . . . . . .
• IAS-MACH CONVERSION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4.14
4.15
4.16
4.17
4.05
4.06
4.07
4.08
4.09
4.10
4.11
4.12
4.13
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OPS DATA
REV 21
SEQ 001
5.00
CONTENTS
 SEVERE TURBULENCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• HYD ARCHITECTURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
• FLT CTL ARCHITECTURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5.01
5.02
5.03
• REQUIRED EQUIPMENT FOR CAT 2 AND CAT 3 . . . . . . . . . . . .
5.04
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SUPPLEMENTARY INFORMATION
A340-600
VERT
SPD
WIND
SPD
KPH
KTS
259
140
200
1
2
314
170
400
2
4
333
180
600
3
6
390
210
800
4
8
450
243
1000
5
10
500
270
1400
7
14
593
320
1600
8
16
834
450
2000
10
20
1019
550
2400
12
24
1112
600
3000
15
29
3400
17
33
4000
20
39
CLOUD CEILING
M
VI6 ALL
A
SEQ VAA
CONVERSIONS
AIRSPEED
Appendix
REV 00
FT
FT/MIN M/SEC
KTS
30
100
50
97
40
130
60
117
50
160
70
136
60
200
80
155
100
330
90
175
200
660
100
195
VIRGIN ATLANTIC AIRWAYS REVISION 01 / 01 July 2002
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MM
REV 00
Appendix
B
ALTIMETER SETTING CONVERSION SEQ VAA
MBS
MM
MBS
MM
MBS
MM
MBS
MM
MBS
590
786.6
630
839.9
670
893.2
710
946.5
750
999.9
1
787.9
1
841.2
1
894.5
1
947.9
1 1001.2
2
789.2
2
842.6
2
895.9
2
949.2
2 1002.5
3
790.6
3
843.9
3
897.2
3
950.5
3 1003.9
4
791.9
4
845.2
4
898.5
4
951.8
4 1005.2
5
793.2
5
846.6
5
899.9
5
953.2
5 1006.5
6
794.6
6
847.9
6
901.2
6
954.5
6 1007.9
7
795.9
7
849.2
7
902.5
7
955.9
7 1009.2
8
797.2
8
850.5
8
903.9
8
957.2
8 1010.5
9
798.6
9
851.9
9
905.2
9
958.5
9 1011.9
600
799.9
640
853.2
680
906.5
720
959.9
760 1013.2
1
801.2
1
854.5
1
907.9
1
961.2
1 1014.5
2
802.6
2
855.9
2
909.2
2
962.5
2 1015.9
3
803.9
3
857.2
3
910.5
3
963.9
3 1017.2
4
805.2
4
858.5
4
911.9
4
965.2
4 1018.5
5
806.6
5
859.9
5
913.2
5
966.5
5 1019.9
6
807.9
6
861.2
6
914.5
6
967.9
6 1021.2
7
809.2
7
862.5
7
915.9
7
969.2
7 1022.5
8
810.6
8
863.9
8
917.2
8
970.5
8 1023.9
9
811.9
9
865.2
9
918.5
9
971.9
9 1025.2
610
813.2
650
866.5
690
919.9
730
973.2
770 1026.5
1
814.6
1
867.9
1
921.2
1
974.5
1 1027.9
2
814.9
2
869.2
2
922.5
2
975.9
2 1029.2
3
4
817.2
818.6
3
4
870.5
871.9
3
4
923.9
925.2
3
4
977.2
978.5
3 1030.5
4 1031.9
5
819.9
5
873.2
5
926.6
5
979.9
5 1033.2
6
821.2
6
874.5
6
927.9
6
981.2
6 1034.5
7
822.6
7
875.9
7
929.2
7
982.5
7 1035.9
8
823.9
8
877.2
8
930.5
8
983.9
8 1037.2
9
825.2
9
878.5
9
931.9
9
985.2
9 1038.5
620
826.6
660
879.9
700
933.2
740
986.5
780 1039.9
1
827.9
1
881.2
1
934.5
1
987.9
1 1041.2
2
829.2
2
882.5
2
935.8
2
989.2
2 1042.5
3
4
830.6
831.9
3
4
883.9
885.2
3
4
937.2
938.5
3
4
990.5
991.9
3 1043.9
4 1045.2
5
833.2
5
886.5
5
939.9
5
993.2
5 1046.5
6
834.6
6
887.9
6
941.2
6
994.5
6 1047.9
7
835.9
7
889.2
7
942.5
7
995.9
7 1049.2
8
837.2
8
890.5
8
943.8
8
997.2
8 1050.5
9
838.6
9
891.9
9
945.2
9
998.5
9 1051.9
VIRGIN ATLANTIC AIRWAYS REVISION 01 / 01 July 2002
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SUPPLEMENTARY INFORMATION
A340-600
FREQUENCIES
Virgin
Company
Freq
(MHz)
Ground
Handling
Freq
(MHz)
AMS EHAM
131.625
ANU TAPA
130.050
BGI
130.200
TBPB
Callsign
131.150
BOS KBOS
131.250
CPT
FACT
129.870
DEL
VIDP
131.150
CAMBATA
DUB EIDW
131.500
AER LINGUS
DXB OMDB
131.600
EWR KEWR
131.250
GND TGPY
131.625
HAV MUHA
126.900
HKG VHHH
131.150
IAD
KIAD
130.075
JFK
KJFK
131.250
JNB
FAJS
131.240
LAS KLAS
129.775
129.000
LGW EGKK
131.425
LHR EGLL
131.425
LOS DNMM
118.300
MAN EGCC
131.425
MCO KMCO
130.275
MIA
130.275
KMIA
Appendix
SEQ VAA
Notes
CAMBATA
Aviation Services of Grenada
HIAS
HIAS FLIGHT OPERATIONS
SWISSPORT
129.150ANZ Eng. 129.600 N/W
122.050
GROUNDSTAR
131.850
DELTA TOWER
129.150 BA Eng.
NAS MYNN
129.800
NRT RJAA
130.900
UNITED
PVG ZSPD
129.800
DONG HAI
130.500 as alternate
130.850
SWISSPORT
129.700 BA Engineering
SYD YSSY
129.600
MENZIES
TAB TTCP
130.700
SERVISAIR
UVF TLPL
131.400
SFO KSFO
VI6 ALL
130.275
C
KLM OPS
BOM VABB
LAX KLAX
REV 00
NAS FLT SERVICES
PENAUILLE SERVISAIR
CARRIBEAN DISPATCH
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SUPPLEMENTARY INFORMATION
A340-600
REV 00
Appendix
SEQ VAA
CRUISING LEVELS
D
U.S.S.R. CRUISING LEVELS
< WEST
EAST >
1,200
1,800
2,400
3,000
3,600
4,200
4,800
5,400
6,000
6,600
m
m
m
m
m
m
m
m
m
m
3,900
5,900
7,900
9,800
11,800
13,800
15,700
17,700
19,700
21,700
ft
ft
ft
ft
ft
ft
ft
ft
ft
ft
900
1,500
2,100
2,700
3,300
3,900
4,500
5,100
5,700
6,300
m
m
m
m
m
m
m
m
m
m
3,000
4,900
6,900
8,900
10,800
12,800
14,800
16,700
18,700
20,700
ft
ft
ft
ft
ft
ft
ft
ft
ft
ft
7,200
7,800
8,600
9,600
10,600
11,600
13,100
m
m
m
m
m
m
m
23,600
25,600
28,200
31,500
34,800
38,100
43,000
ft
ft
ft
ft
ft
ft
ft
6,900
7,500
8,100
9,100
10,100
11,100
12,100
m
m
m
m
m
m
m
22,600
24,600
26,600
29,900
33,100
36,400
39,700
ft
ft
ft
ft
ft
ft
ft
CHINA CRUISING LEVELS
< WEST
EAST >
600
1,200
1,800
2,400
3,000
3,600
4,200
4,800
5,400
m
m
m
m
m
m
m
m
m
2,000
3,900
5,900
7,900
9,800
11,800
13,800
15,700
17,700
ft
ft
ft
ft
ft
ft
ft
ft
ft
6,000
6,600
7,200
7,800
8,400
9,600
10,800
12,000
m
m
m
m
m
m
m
m
19,700
21,700
23,600
25,600
27,600
31,500
35,400
39,400
ft
ft
ft
ft
ft
ft
ft
ft
900
1,500
2,100
2,700
3,300
3,900
4,500
5,100
5,700
m
m
m
m
m
m
m
m
m
6,300
6,900 m
m
7,500 m
8,100 m
9,000 m
10,200 m
11,400 m
12,600 m
3,000
4,900
6,900
8,900
10,800
12,800
14,800
16,700
18,700
ft
ft
ft
ft
ft
ft
ft
ft
ft
20,700
22,600 ft
ft
24,600 ft
26,600 ft
29,500 ft
33,500 ft
37,400 ft
41,300 ft
VIRGIN ATLANTIC AIRWAYS REVISION 03 / 22 May 2003
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SUPPLEMENTARY INFORMATION
A340-600
Appendix
REV 00
SEQ VAA
AIRCRAFT INFORMATION
E
Applicable to ALL A340-642
G-VGOA (371
G-VATL (376)
G-VSHY (383)
G-VMEG (391)
G-VOGE (416)
G-VFOX (449)
G-VEIL (575)
G-VSSH (615)
G-VNAP (622)
G-VGAS (639)
G-VWKD (706)
G-VBLU (723)
G-VWIN (736)
G-VFIT (753)
G-VFIZ (764)
G-VYOU (765)
s
g
k
s
g
k
g
k
0
2
,
9
6
3
0
0
,
8
6
3
0
0
,
9
5
2
t
h
g
i
t
h e
g
W
i
e ff
W O
y e
x
a
k
T a
T
m m
u u
m
m
i
i
x x
a a
M M
VI6 ALL
s
g
k
0
0
,
5
4
2
s
g
k
0
4
,
2
5
1
t
h
g
i
e
W
l
e
u
F
o *
rZ ity
e
c
a
m m p
u u a
C
m
m
i
i
x x le
a a u
M M F
t
h
g
i
e
W
g
n
i
d
n
a
L
s
t
k
0
1
)
g
n
i
d
n
a
L
d
n
a
ff
O
e
k
a
T
(
d
n
i
w
ilT
a
m
u
m
i
x
a
M
d
e
d
u
l
c
n
i
t
s
u
g
s
t
k
5
3
d
e
d
u
l
c
n
i
t
s
u
g
s
t
k
7
3
)f
f
O
e
k
a
T
(
)
g
n
i
d
n
a
L
(
e
d
t
a
rt
s
n
o
m
e
D
d
n
i
w
s
s
ro
C
e
d
t
a
rt
s
n
o
m
e
D
d
n
i
w
s
s
ro
C
m
u
m
i
x
a
M
m
u
m
i
x
a
M
.
e
rt
il
r
e
p
s
g
k
5
8
7
.
0
f
o
y
ti
s
n
e
d
l
e
u
f
a
n
o
d
e
s
a
B
*
VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006
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SUPPLEMENTARY INFORMATION
A340-600
STANDARD FUELLING
REV 00
Appendix
SEQ VAA
F
FUEL TANK QUANTITY (Kgs)
Valid for all fuel SGs between 0.74 and 0.88 kgs/litre
TOTAL
FUEL
TRIM
TOTAL
FUEL
TRIM
81800
82000
83000
84000
85000
86000
87000
88000
89000
90000
91000
92000
0
14
84
153
223
293
363
433
502
572
642
712
126000
127000
128000
129000
130000
131000
132000
133000
134000
135000
136000
137000
3694
3826
3958
4091
4223
4355
4487
4619
4751
4883
5015
5147
93000
94000
95000
96000
97000
98000
99000
100000
101000
102000
103000
104000
105000
106000
107000
108000
109000
110000
111000
112000
113000
114000
115000
116000
116200
117000
118000
119000
120000
121000
122000
123000
124000
125000
781
851
921
991
1060
1130
1200
1270
1340
1409
1479
1549
1619
1688
1758
1828
1898
1967
2037
2107
2177
2247
2316
2386
2400
2506
2638
2770
2902
3034
3166
3298
3430
3562
138000
139000
140000
141000
142000
142700
143000
144000
145000
146000
147000
148000
149000
150000
151000
152000
153000
154000
155000
156000
157000
158000
159000
160000
161000
162000
163000
164000
165000
166000
167000
168000
169000
169700
5279
5411
5543
5675
5808
5900
5912
5952
5992
6032
6072
6112
6152
6192
6232
6271
6311
6351
6391
6431
6471
6511
6551
6591
6631
6671
6711
6751
6791
6831
6871
6911
6951
6978
VIRGIN ATLANTIC AIRWAYS REVISION 05 / 05 December 2003
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SUPPLEMENTARY INFORMATION
A340-600
DERATE CLIMB
REV 00
Appendix
SEQ VAA
G
There are two initial thrust reductions, De-rate 1 and De-rate 2.
De-rate 1 is a 10% reduction of full climb thrust and De-rate 2 is a 15%
reduction. At altitudes (above 30,000 ft) the de-rate climb is identical
to the max climb rating. For temperatures below ISA +10° there is a
progressive transition from De-rate climb to max climb between
26,000 ft and 30,000 ft for DCLB 1 and between 24,000 ft and 30,000
ft for DCLB2. With Ambient temps >ISA +10° the altitudes are lower.
De-rate climb can be selected on the PERF CLB Page, by inserting
'D1' or 'D2' in position (1R) on the CLB Page.
After analysis of the data the following is a guide to the use of De-rate
Climb.
Ground OAT
D1
D2
<ISA +10°
<360T
<340T
<ISA +15°
<355T
<335T
<ISA +20°
<350T
<330T
VI6 ALL
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SUPPLEMENTARY INFORMATION
A340-600
REDUCED TAKE-OFF THRUST
REV 00
Appendix
SEQ VAA
H
Reduced Take-Off Thrust may be used at the Captain's discretion
and is referred to as Flexible Take-Off Thrust. Flexible Thrust may be
used
the actual
weight
is lower
than
the RTOW,
except
whenwhen
prohibited
by thetake-off
exceptions
listed
below.
Thrust
reduction
must
not exceed 40% of the full rated take-off thrust. Use of reduced thrust,
where possible, will assist engine condition and make a significant
contribution to reducing the rate of engine failure. The engines may be
opened up to full 'Go-around thrust at any time after V1 is attained
should the need arise.
Reduced Take-Off Thrust (Flexible Trust) must not be used when:
(a)
The corrected 'FLEX' temperature (CT) is higher than ISA
+60°C or lower than 'TREF' (Reference Temperature) or lower
than ambient temperature.
(b)
The runway is affected by snow, slush, standing water or ice, or
suspected of having a marginal braking capability.
(c)
Significant windshear conditions are anticipated.
(d)
Operating with landing gear extended.
(e)
One or more brake(s) inoperative.
(f)
One or more thrust reversers are inoperative.
(g)
Ground spoilers inoperative.
(h)
One tachometer inoperative.
(i)
Generalised or non specific RTOW tables are used.
A calculated RTOW of more than maximum structural can be used for
Flexible Thrust calculations.
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A340-600
SUPPLEMENTARY INFORMATION
TAKE-OFF DATA CALCULATION
(TODC)
Item
Definition
AIRPORT *
Airport ICAO code
RUNWAY *
Runway
REV 00
Appendix
I
SEQ VAA
Example
KBOS
22L
Note:- For Taxyway/Holding Point start of roll positions,
suffix the Runway designator Taxyway/Holding
Point designator. (e.g. 21LN3).
DIRECTION *
Wind Direction (°)
190
SPEED *
Wind Speed (kts)
009
OAT *
Outside Air Temp = -50 to 55
12
QNH *
QNH
Note:- Range 0920 to 1070 implies hPa.
Range 2700 to 3200 implies Hg.
i.e. “2745” = 27.45 Hg.
1020
%MAC
% Mean Aerodynamic Chord
Note:- 170 = %MAC 17.0.
170 is the Standard CG position for Take-Off
calculations for the A340-600.
Default = 170.
170
AZFW *
Actual Zero Fuel Weight (kg)
245000
ATOW *
Actual Take-Off Weight (kg)
308500
CONDTN
Runway Condition
0 = Dry
1 = Wet
2 = Standing Water
0
3 = Slush
4 = Compact Snow
5 = Wet Snow
6 = Dry Snow
7 = Dry Ice
8 = Wet Ice
9 = Very Dry Snow
Default = 0.
When selecting options 2 to 9,
REVERS must be set to 0.
SHORTENING
Shortened Runway (metres)
“B” prefix denotes the runway has been
B0800
shortened at the Beginning/Start of Roll end
of the runway. “E” suffix denotes the runway
has been shortened at the Lift-Off End of the
runway. Range – 0001 to 2000 metres.
Default = Blank spaces.
DEPTH
VI6 ALL
Contaminant Depth (mm)
Depth not required for items 0, 1, 4, 7 or 8 above.
Default N/A (see above).
05
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A340-600
Item
SUPPLEMENTARY INFORMATION
TAKE-OFF DATA CALCULATION
(TODC)
REV 00
Appendix
J
SEQ VAA
Definition
Example
BRK ACTION
Runway Braking Action
Note:- 0 = Friction Coefficient
1 = GOOD
2 = MEDIUM to GOOD
3 = MEDIUM
4 = MEDIUM to POOR
5 = POOR
Enter “0” if Friction Coefficient reported.
Then enter Friction Coefficient (see below).
Default = 1.
1
FC
Friction Coefficient
Note:- Range from 16 to 70. e.g 21 = FC 0.21.
Default = Blank spaces.
21
FLAPS *
Take-Off
Note:- 1
= Conf Flaps/Configuration
1+F, 2 = Conf 2, 3 = Conf 3.
Default = 3.
3
AIR COND
Air Conditioning
Note:- 0 = Off. 1 = On.
Default = 0.
0
REVERS
Reverse Thrust considered
Note:- 0 = ALL OK. 1 = 1 Inboard Inop.
2 = 1 Outboard Inop. 3 = All Inop
Default = 3.
When CONDTN is set to 2 to 9, REVERS
3
must be set to 0.
ANT ICE
Anti-Ice considered
0
Note:- 0 = Off. 1 = Engine AI On. 2 = Engine & Wing AI On.
Default = 0.
BRAKES
Brakes
Note:- 0 = OK. 1 = 1 Inop. 2 = 2 Inop.
Default = 0.
0
L/GEAR
Landing Gear
Note:- 0 = OK. 1 = Extended
Default = 0.
0
WHEEL TACHO Wheel Tachometer
Note:- 0 = OK. 1 = 1 Inop.
Default = 0.
0
GRND IDLE
0
Ground Idle
Note:- 0 = OK. 1 = Inop.
Default = 0.
VIRGIN ATLANTIC AIRWAYS REVISION 10 / 01 May 2005
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A340-600
SUPPLEMENTARY INFORMATION
TAKE-OFF DATA CALCULATION
(TODC)
Item
REV 00
Appendix
K
SEQ VAA
Definition
Example
ENG ANT-ICE
Engine Anti-Ice Valve Position
VALVE POSN
Note:- 0 = OK. 1 = Open.
Default = 0.
0
ENGINES
0
Engines Inop
Note:- 0 = None. 1 = 3 Engine Ferry
Default = 0.
ALT RUNWAY
Alternate Runways
Note:- 0 = No. 1 = Yes.
If “1” is inserted a calculation will be done for all
runways for the specified airport held in the
TODC database.
Default = 0.
0
GROUND
SPOILER
0
Ground Spoilers
Note:- 0 = OK. 1 = 1 Pair Inop.
2 = 2 Pairs Inop. 3 = All Inop.
Default = 0.
* Mandatory Input.
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REV 24
NORMAL CHECKLIST
A340-600
7.01
SEQ 205
BEFORE START
COCKPIT PREP . . . . . . .COMPLETE (BOTH)
GEAR PINS and COVERS . . . . . .REMOVED
SIGNS . . . . . . . . . . . . . . . . . . . . . . . . .ON / AUTO
APPROACH
BRIEFING . . . . . . . . . . . . . . . . . . . . . . CONFIRM
ECAM STATUS . . . . . . . . . . . . . . . . . . . . CHECK
SEAT BELTS . . . . . . . . . . . . . . . . . . . . . . . ON
ADIRS
. . . . . . . . . .. .. .. .. .. .........._________
. . . . . . . . .NAV
FUEL QUANTITY
KG
TO DATA / DCLB . . . . . . . _____SET (BOTH)
BARO REF . . . . . . QNH_______SET (BOTH)
MINIMUMS.
. .__________ SET
BARO . . . . . .. . QNH__________
SET(BOTH)
(BOTH
WINDOWS/DOORS. . .CLOSED/ARMED (BOTH)
BEACON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
THR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . .IDLE
PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . .SET
AFTER START
ANTI ICE . . . . . . . . . . . . . . . . . . . . . . . .AS RQRD
ECAM STATUS . . . . . . . . . . . . . . . . . . . . CHECK
TRIMS . . . . . . . . . . . . . . . . __________ SET
BEFORE T.O.
FLIGHT CONTROLS . . . . CHECKED (BOTH)
FLT INST . . . . . . . . . . . . . . . CHECKED (BOTH)
BRIEFING/CLEARANCE . . . . . .CONFIRM
FLAPS . . . . . . . . . . . . . . ________ SET (BOTH
T.O. SPEEDS/
FLX TEMP . . . . .____ ____/____(BOTH)
ECAM MEMO . . . . . . . . . . . . . . . .T/O NO BLUE
.
.
.
.
.
AUTO BRK MAX
SIGNS ON
SPLRS ARM
FLAPS TO
TO CONFIG NORM
CABIN . . . . . . . . . . . . . . . . . . . . . . . READY/ADVISE
LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
PACKS . . . . . . . . . . . . . . . . . . . . . . ON APU/OFF
RADAR/TCAS/PWS . . . . . AS RQRD/SET/AUTO
AFTER T.O./CLIMB
LDG GEAR . . . . . . . . . . . . . . . . . . . . . . . . UP
FLAPS . . . . . . . . . . . . . . . . . . . . . . .RETRACTED
PACKS / APU . . . . . . . . . . . . . . . . . . . . ON/OFF
BARO REF . . . . . . . . . ________ SET (BOTH)
LANDING
A/THR . . . . . . . . . . . . . . . . . . . . . .SPEED/OFF
ECAM MEMO . . . . . . . . . . . . . . .LDG NO BLUE
.
.
.
.
L/G/ DOWN
SIGNS ON
SPLRS ARM
FLAPS SET
CABIN . . . . . . . . . . . . . . . . . . . . . . . . . . . . READY
SPOILERS . AFTER
. . . . . . . . .LANDING
. . . . . . . . . . DISARMED
FLAPS . . . . . . . . . . . . . . . . . . . . . . .RETRACTED
RADAR/PWS . . . . . . . . . . . . . . . . . . OFF/OFF
APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .START
PARKING
APU BLEED . . . . . . . . . . . . . . . . . . . . . . . . ON
ENGINES . . . . . . . . . . . . . . . . . . . . . . . . . OFF
SEAT BELTS . . . . . . . . . . . . . . . . . . . . . . . OFF
EXT LT . . . . . . . . . . . . . . . . . . . . . . . . . AS RQRD
FUEL PUMPS . . . . . . . . . . . . . . . . . . . . . . OFF
CHOCKS and PARK BRAKE . . . . AS RQRD
SECURING AIRCRAFT
TCAS. . . . . . . . . . . . . . . . . . . . . . . . . . . STBY
ADIRS . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
OXYGEN . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
APU BLEED . . . . . . . . . . . . . . . . . . AS RQRD
EMER EXIT LT . . . . . . . . . . . . . . . . . . . . . . .OFF
NO SMOKING . . . . . . . . . . . . . . . . . . . . . . .OFF
BAT 1 + 2 + APU BAT . . . . . . . . . . . . .AS RQRD
TECH LOG . . . . . . . . . . .. . . . . . . . COMPLETED
ON GROUND EMER / EVACUATION
-
AIRCRAFT/PARKING BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . STOP/ON
CM1
-
∆P
ATC (VHF 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY
(only if MAN CAB PR has been used) . . . . . . . . . . . . . CHECK ZERO
CM1
CM1
IF ∆P IS NOT ZERO SELECT MANUAL MODE AND V/S CTL FULL UP TO FULLY OPEN THE OUTFLOW VALVE.
-
ALL ENG MASTER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
FIRE P/Bs (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
AGENTS (ENG and APU) . . . . . . . . . . . . . . . . . . . . . . . . . . DISCHARGE
EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE
BAT 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
TAKEOFF CG
TRIM POS
13/16
24
20
6
5
4
28
3
32
2
36
1
CM1
CM1
CM1
CM1
OFF
40/44
0
VIRGIN ATLANTIC AIRWAYS REVISION 09 / 01 April 2005
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CROSS REFERENCE TABLE
THIS TABLE GIVES, FOR EACH AIRCRAFT INCLUDED IN THE MANUAL, THE CROSS REFERENCE
BETWEEN :
- THE MANUFACTURING SERIAL NUMBER (MSN) WHICH APPEARS IN THE LIST OF EFFECTIVE PAGES
- THE REGISTRATION NUMBER OF THE AIRCRAFT AS KNOWN BY AIRBUS INDUSTRIE.
---------------------------------------------------------------------------MSN
REGISTRATION
----------------------------------------------------------------------------
0371
G-VGOA
0376
G-VATL
0383
G-VSHY
0391
G-VMEG
0416
G-VOGE
0449
G-VFOX
0575
G-VEIL
0615
G-VSSH
0622
G-VNAP
0639
G-VGAS
0706
G-VWKD
0723
G-VBLU
0736
G-VWIN
0753
G-VFIT
0764
G-VFIZ
0765
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GENERAL INFORMATION
A340-600
RECORD OF TEMPORARY REVISIONS
MSN Nos: 0371 - G-VGOA
20 MAR 06
SEQ VAA
TRs
0376 - G-VATL
0383 - G-VSHY
0391 - G-VMEG
0416 - G-VOGE
0449 - G-VFOX
0575 - G-VEIL
0615 - G-VSSH
0622 - G-VNAP
0639 - G-VGAS
0736 - G-VWIN
0753 - G-VFIT
0706 - G-VWKD
0723 - G-VBLU
0764 - G-VFIZ
0765 - G-VYOU
No.
Title
Applicable
Aircraft
183-1B
COCKPIT DOOR LOCKING SYSTEM JAM
0371-0575
200-1H
CDSS SMOKE FROM LCD MONITOR
232-2B
ENGINE FUEL FEED PIPE RUPTURE WITHIN FUEL TANK
234-1A
"SMOKE CABVIDEO 1 (2)(3)(4) SMOKE" ECAM WARNING
ALL
235-1A
"SMOKE VIDEO 1 (2)(3)(4) DET FAULT" ECAM CAUTION
ALL
236-1A
"COND IFE BAY VENT FAULT" ECAM CAUTION, or "SMOKE
IFE BAY DET FAULT" ECAM CAUTION
ALL
243-1B
FUEL 1 (2) FAULT/FUEL MONITORING
258-1A
DISPLAY UNIT FAILURE - INVALID DISPLAY UNIT
ALL
259-1A
PERIODIC RESET OF ALL DISPLAY UNITS
ALL
261-1A
ABNORMAL PROCEDURES - FUEL WING TANKIMBALANCE
ALL
0416
0371-0639
0371-0706
New or revised Temporary Revisions included in this revision are highlighted in bold type.
VIR ALL
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QUICK REFERENCE
HANDBOOK
A340-600
VAA PAGE
LEP
LIST OF EFFECTIVE PAGES AMENDED
OR ADDED BY VIRGIN ATLANTIC AIRWAYS
New or revised pages included in this revision are highlighted in bold text.
Page
MSN No.
Effective Date
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
01 Jul 02
20 Mar 06
20 Mar 06
20 Mar 06
20 Mar 06
20 Mar 06
20 Mar 06
As dated
01 May 05
26 Jul 04
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
22 Jul
May02
03
01
15 Aug 05
20 Mar 06
20 Mar 06
20 Mar 06
20 Mar 06
01 May 05
20 Mar 06
20 Mar 06
01 May 05
01 May 05
15 Aug 05
15 Aug 05
2.09
2.10A
2.11A
3.00
3.01
3.02
VS LEP
VS Appendix A
VS Appendix B
VS Appendix C
VS Appendix D
VS Appendix E
VS Appendix F
VS Appendix G
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
ALL
01
26 Jul
Jul 02
04
15 Aug 05
01 Jul 02
15 Aug 05
01 May 05
20 Mar 06
01 Jul 02
01 Jul 02
20 Mar 06
22 May 03
15 Aug 05
05 Dec 03
15 Aug 05
VS
VS Appendix
Appendix H
I
VS Appendix J
VS Appendix K
7.01
ALL
ALL
ALL
ALL
ALL
05
15 Dec
Aug 03
05
01 May 05
12 Mar 04
01 Apr 05
0.00
0.00B
0.00C
0.00D
0.00E
0.00F
0.00G
VSRecord of TR's
1.00
1.05
1.10
1.11
1.12
1.15
1.16
1.18
1.19
1.20
1.22
1.24
1.25
1.26
2.00
2.08A
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VIRGIN ATLANTIC AIRWAYS REVISION 12 / 20 March 2006
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QUICK REFERENCE HANDBOOK
REV025A
LIST OF EFFECTIVE PAGES (LEP)
M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA----M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA-----------------------EFFECTIVITY-----------------------------------------------------------------------------------------0 .00
001 REV019
ALL
0 .00A
001 REV023
ALL
0 .01
0 .02
001 REV025
001 REV025
ALL
LIST OF CODES
LIST OF CODES
0 .02A
001 REV025
ALL
LIST OF CODES
0 .03-
001 REV025
ALL
LIST OF TEMPORARY REVISIONS
0 .04-
001 REV025
ALL
CROSS REFERENCE TABLE
0 .06-
001 REV025
ALL
LIST OF EFFECTIVE PAGES
0 .07-
001 REV025
ALL
LIST OF MOD/MP/SB
1 .00
001 REV024
ALL
1 .01
1 .02
100
200
1 .03
1 .04
ALL
302 REV025
100 REV025
ALL
40624+41300+47000
47002
1 .05
1 .06
001 REV025
100 REV025
ALL
CODE 0080
1 .06A
001 REV025
ALL
1 .06B
001 REV025
ALL
1 .07
1 .08
300 REV025
302 REV025
ALL
M:40624+41300+47000
40624+41300+47000
1 .09
300
M:40624+41300+47000
1 .10
100ALL
REV021
47002
1 .11
1 .12
102 REV025
100 REV023
ALL
49026
CODE 0008
1 .13
1 .14
102 REV025
102 REV024
ALL
47000
47002
1 .15
1 .16
205 REV024
205 REV025
ALL
CODE 0066
CODE 0066
1 .17
1 .18
104 REV025
205 REV024
ALL
47002
CODE 0066
1 .19
1 .20
205 REV025
001 REV024
ALL
CODE 0066
1 .21
1 .22
100 REV025
200 REV025
ALL
46324=52992
CODE 0066
1 .23
1 .24
100 REV025
200 REV024
ALL
46324=52992
CODE 0066
1 .25
001 REV024
ALL
STD=40257=40379
2 .00
402
REV025 46257+46290+47002+50014
0371-0615
2 .00
505
REV025 CODE 0078
0622-0765
2 .00A
100 REV025
ALL
REV019
REV022
REV025
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CODE:0009
47002
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REV025A
LIST OF EFFECTIVE PAGES (LEP)
M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA----M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA-----------------------EFFECTIVITY-----------------------------------------------------------------------------------------2 .00B
001
REV024
ALL
2 .01
2 .02
102
102
REV022
REV025
ALL
2 .03
2 .04
100
210
REV019
REV013
2 .05
2 .06
100
102
REV022
REV022
ALL
47002
47002
2 .06A
160
REV025
ALL
M:47002/RR
2 .06B
060
REV022
ALL
RR 556-61
2 .07
2 .08
100
100
REV025
REV025
ALL
47002
47000
2 .08A
102
REV025
ALL
47000
2 .09
2 .10
100
105
REV025
REV025
47002
47000
2 .11
105
2 .11
200
REV024 CODE 0076
0622-0765
2 .11A
001
REV025
ALL
2 .12
001
REV021
ALL
2 .13
2 .14
100
100
REV021
REV022
ALL
M:47002
47002
2 .15
2 .16
100
100
REV025
REV021
ALL
47002
47002
2 .17
2 .18
100
300
REV023 49192=52306=47002+519 13
REV023 CODE 0048
0622-0765
2 .17
2 .18
110
300
REV023 M:47002
REV023 CODE 0048
0371-0615
2 .19
2 .20
100
001
REV025 M:47002
REV023
0371-0615
2 .19
2 .20
100
100
REV025 M:47002
REV023 CODE 0077
0622-0765
2 .20A
001
REV025
ALL
2 .20B
100
REV025
ALL
CODE 0058
2 .21
2 .22
123
100
REV025
REV025
ALL
CODE 0069/ E556-61
CODE 0069
2 .23
100
REV025
ALL
CODE 0069
2 .23A
043
REV025
ALL
556-61
2 .23B
043
REV025
ALL
556-61
2 .24
001
REV025
ALL
2 .25
2 .26
100
150
REV021
REV025
ALL
50014
M:47000
M:47002=49144
M:46257+46290
ALL
ALL
REV024 CODE 0075
0371-0615
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46257
M:50968/RR
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QUICK REFERENCE HANDBOOK
REV025A
LIST OF EFFECTIVE PAGES (LEP)
M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA----M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA-----------------------EFFECTIVITY-----------------------------------------------------------------------------------------2 .27
2 .28
050 REV021
050 REV023
ALL
RR
RR
2 .29
140 REV024
ALL
47000/RR556-61
2 .29A
160 REV022
ALL
M:47000/RR 556-61
2 .29B
160 REV022
ALL
M:47000/RR 556-61
2 .30
001 REV024
ALL
2 .31
2 .32
001 REV021
100 REV021
ALL
2 .33
2 .34
001 REV021
001 REV021
ALL
2 .35
2 .36
100 REV025
200 REV025
ALL
40259=40512
43078+47002
2 .37
2 .38
300
300
46742+47002+47921
M:45748+47002+50616
2 .39
2 .40
ALL
020 REV024 RR
100 REV022 47000=44495+47000
0371-0449
2 .39
2 .40
120
100
2 .41
2 .42
105 REV025
105 REV025
ALL
47000
47000
2 .43
2 .44
105 REV025
001 REV025
ALL
47000
3 .00
001 REV011
ALL
.01
3 .02
200 REV022
REV024 47244
CODE 0125
102
0371-0376 0391-0416 0575-0765
3 .01
3 .02
300 REV024 CODE 0126
102 REV022 47244
0383 0449
3 .03
3 .04
050 REV025
100 REV025
ALL
3 .05
3 .06
001 REV025
001 REV025
ALL
3 .07
3 .08
001 REV025
001 REV025
ALL
3 .09
3 .10
100 REV025
001 REV014
ALL
4 .00
001 REV010
ALL
4 .01
4 .02
178 REV025
210 REV022
ALL
47000=44495+47000/RR556
RR556/47000+40624
4 .03
4 .04
210 REV022
210 REV023
ALL
RR556/47000+40624
M:40624+47000/RR556
4 .05
4 .06
140
140
REV021 RR556/47000
REV021 RR556/47000
0371-0622
4 .05
4 .06
240
240
REV024 47000+50655/RR 556
REV024 47000+50655/RR 556
0639-0765
REV025
REV025
REV024 M:MP S17972/RR
REV022 47000=44495+47000
0575-0765
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RR=SIA/RR
46459
47002=47002/ACA/SIA
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QUICK REFERENCE HANDBOOK
REV025A
LIST OF EFFECTIVE PAGES (LEP)
M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA----M ---PAGE--- SEQ- --REV-- ----VALIDATION CRITERIA-----------------------EFFECTIVITY-----------------------------------------------------------------------------------------4 .07
4 .08
140
140
REV021 RR556/47000
REV023 RR556/47000
0371-0622
4 .07
4 .08
240
240
REV024 47000+50655/RR 556
REV024 47000+50655/RR 556
0639-0765
4 .09
140
4 .10
140
REV023 M:47000/RR556
0371-0622
4 .09
4 .10
140
240
REV022 RR556/47000
REV024 47000+50655/RR 556
0639-0765
4 .11
4 .12
120
105
REV023 47000/RR 556
REV022 M:47002
0371-0622
4 .11
4 .12
240
105
REV024 47000+50655/RR 556
REV022 M:47002
0639-0765
4 .13
4 .14
120
120
REV024 47000/RR 556
REV023 47000/RR 556
0371-0622
4 .13
4 .14
120
240
4 .15
4 .16
120
001
4 .15
4 .16
240
001
REV024 47000+50655/RR 556
REV010
0639-0765
4 .17
001
REV011
ALL
5 .00
001
REV021
ALL
5 .01
5 .02
100
100
REV025 RR556/47000
REV023 M:47002
0371-0622
5 .01
250
5 .02
100 0639-0765
REV023 M:47002
5 .03
5 .04
100
102
REV022
REV024
ALL
47002
47002
7 .01
205
REV024
ALL
CODE:0056
REV022
REV024
REV024
47000/RR 556
47000+50655/RR 556
0639-0765
REV023 47000/RR 556
REV010
0371-0622
REV025
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47000+50655/556-61
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QRH
VOLUME :
3
LIST
MOD/MP/SB AFFECTING THE MANUAL
OF
QUICK REFERENCE HANDBOOK
REVISION : 025A
M
V REV
MOD
T
MP
TITLE
SB
. 023
VALIDITY
...... S17972
...........
AIR-NACELLE TEMPERATURE INDICATING RELOCATE
RRT500 ENGINE FOR A3456-CNFRR26
G-VEIL
G-VSSH
G-VNAP
G-VGAS
G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
. 021
40259
......
...........
EQUIPMENT/FURNISHINGS-CRE W REST
COMPARTMENT-INSTALL STRUCTURAL
PROVISIONS
ALL
. 020A 40624
......
...........
INDICATING/RECORDING SYSTEMS-FMGECREPLACE METERS BY FEET
ALL
. 020A 41300
......
...........
WINGS-GENERAL-DEFINE A340 GROWTH
VERSION
ALL
. 020A 43078
......
...........
FLIGHT CONTROLS - CHANGE WIRING OF
FCPC1 AND FCSC1 FAULT INDICATOR LIGHTS
ALL
. 020A 44482
......
...........
ICE AND RAIN PROTECTION WINDSHIELD RAIN PROTECTION DEACTIVATE RAIN REPELLENT SYSTEM
ALL
. 020A 44495
......
...........
AUTO FLIGHT - FMGEC - INTRODUCE L6
STD FOR CFMI
ALL
. 020A 44575
......
...........
FUEL - FMCS - FIT FCMC (STAGE 7.1) WITH
CHANGES TO SOFTWARE FOR A330 AND A340
AIRCRAFT
ALL
. 020A 44604
......
...........
FUEL - APU FUEL PUMP SYSTEM - PREVENT
AN ELECTRICAL ESS NETWORK OVERLOAD
(A340)
ALL
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QRH
VOLUME :
3
LIST
MOD/MP/SB AFFECTING THE MANUAL
OF
QUICK REFERENCE HANDBOOK
REVISION : 025A
M
V REV
T
. 021
MOD
MP
TITLE
SB
44754
VALIDITY
......
...........
NAVIGATION - WEATHER RADAR SYSTEM ACTIVATE ALLIED SIGNAL PREDICTIVE
WINDSHEAR FUNCTION
ALL
. 020A 45057
......
...........
INDICATING/RECORDING SYSTEM - FWC DEFINE NEW OEB REMINDER FUNCTION
ALL
. 020A 45509
......
...........
NAVIGATION - MMR - INSTALL COLLINS
MULTI-MODE RECEIVERS PROVIDING ILS
(FM IMMUNE) AND GPS PRIMARY FUNCTION
ALL
. 023
45748
......
...........
OXYGEN - CREW OXYGEN - INSTALL A 115
CU.FT COMPOSITE OXYGEN CYLINDER
ALL
. 022
45897
......
...........
ICE AND RAIN PROTECTION - WINDSHIELD
RAIN PROTECTION - REACTIVATE THE RAIN
REPELLENT SYSTEM
ALL
. 020A 46257 ......
...........
INDICATING/RECORDING SYSTEMS - FWC INSTALL NEW FWC STANDARD L7-0
ALL
. 020A 46290
......
...........
FLIGHT CONTROLS - FCDC - INSTALL FCDC
STANDARD L15/M12
ALL
. 020A 46324
......
...........
NAVIGATION - GPWS - ACTIVATE ENHANCED
GPWS
ALL
. 022
46459
......
31-5011 02
INDICATING/RECORDING SYSTEMS-CENTRAL
WARNING SYSTEMS-PROVIDE NEW AUTO
CALL-OUT CALLED V1
ALL
. 020A 46532
......
...........
INDICATING/RECORDING SYSTEMS - EIS DISPLAY MANAGEMENT COMPUTER - INSTALL
NEW DMC SOFTWARE V110X
ALL
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TITLE
SB
. 020A 46728
VALIDITY
......
...........
NAVIGATION-TCAS-INSTALL ALLIED SIGNAL
CHANGE 7 P/N 066-50000-2220
ALL
. 023
46742
......
...........
INFORMATION SYSTEMS - AIR TRAFFIC AND
INFORMATION MANAGEMENT SYSTEM ACTIVATE ATSU
ALL
. 020A 46893
......
...........
NAVIGATION - MMR - INSTALL COLLINS
MULTI-MODE RECEIVERS P/N 822-1152-121
ALL
. 022
46976
......
30-5001
ICE AND RAIN PROTECTION - WINDSHIELD
RAIN PROTECTION - DE-ACTIVATE RAIN
REPELLENT SYSTEM
. 020A 47000
......
...........
. 020A 47002
......
...........
G-VGOA
G-VATL
G-VMEG
G-VOGE
G-VEIL
G-VSSH
G-VNAP
G-VGAS
G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
GENERAL - PROVIDE BASIC DEFINITION
FOR A340-600
ALL
WINGS - GENERAL - DEFINE BASIC DESIGN
FOR A340-500/600
ALL
. 020A 47110
......
...........
COMMUNICATIONS-GENERAL-IN STALL CEIS
P/N 93N6035 EMERGENCY CONTROL PANEL IN
COCKPIT
ALL
. 022
47244
......
...........
NAVIGATION-STANDBY NAVIGATION SYSTEMSINSTALL SEXTANT AVIONICS INTEGRATED
STANDBY INSTRUMENT SYSTEM (ISIS)
ALL
. 020A 47524
......
...........
INDICATING/RECORDING SYSTEMS-ELECTRONIC
INSTRUMENT SYSTEM - INSTALL NEW DISPLAY
SYSTEM (EIS2) EQTS (DMC/DU/DISKETTES)
ALL
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VALIDITY
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INFORMATION SYSTEMS - ATIMS - INSTALL
ATSU RESET PUSHBUTTON SWITCH FOR FANS
A CONFIGURATION
ALL
. 021
49026
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NAVIGATION - EGPWS - ACTIVATE
OBSTACLE FUNCTION
ALL
. 024
49101
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AIR CONDITIONING-DISTRIBUT ION-INSTALL A
SMOKE DETECTION SYST. FOR VCC CONNECTED
TO THE AIR EXTRACTION SYST.IN DOOR 1 LH
ALL
. 022
50014
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EQUIPMENT/FURNISHINGS - COCKPIT INSTALL AN ARMOURED COCKPIT DOOR
ALL
. 024
50161
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INDICATING/RECORDING SYSTEM - EIS INSTALL NEW EIS2 STANDARD L3-1
(DMC, DU AND DISKS)
ALL
. 024
50242 ......
23-5001 04
COMMUNICATIONS - VIDEO MONITORING INSTALL A COCKPIT DOOR SURVEILLANCE
SYSTEM (CDSS)
ALL
. 022
50246
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FLIGHT CONTROLS - SLAT/FLAP CONTROL
COMPUTER - INTRODUCE SFCC STANDARD
-0508
ALL
. 024
50279
......
...........
ENGINE - GENERAL - DEFINE ENGINE
CONFIGURATION FOR A340-600 AIRCRAFT
TYPE CERTIFICATE
ALL
. 022
50321
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...........
AUTO FLIGHT - FMGEC - INSTALL EIS STD
P2-E3 FOR A340-600
ALL
. 023
50616
......
31-5001
INDICATING/RECORDING SYSTEMS - EIS INTALL NEW EIS2 STANDARD L4 ON
A330/A340 ENHANCED
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ENGINE - GENERAL - INTRODUCE ENHANCED
PERFORMANCE PACKAGE ON RR T500 ENGINES
G-VGAS
G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
. 022
50968
......
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ENGINE FUEL AND CONTROL- FADEC INTRODUCE NEW EEC STD L4.1.3 ON RR
T500 ENGINES
ALL
. 024
51153
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31-5001
INDICATING/RECORDING SYSTEMS - EIS INSTALL NEW EIS2 STANDARD L4-1 CAPABLE
OF ALL LONG RANGE AIRCRAFT
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51315
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AUTO FLIGHT - FMGEC - INSTALL NEW
STANDARD FMGEC P2E5
ALL
. 023
51486
......
32-5018 01
LANDING GEAR - NORMAL BRAKING INTRODUCE BSCU STANDARD S2K
ALL
. 023
51733
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FLIGHT CONTROL - FLIGHT CONTROL PRIMARY
COMPUTER (FCPC) - INSTALL NEW FCPC
SOFTWARE STANDARD W8 ON A340/500-600
ALL
. 024A 51973
......
...........
INDICATING/RECORDING SYSTEMS
- FWC -
INSTALL FWC W4-0 WITH 486 BASED CPU
BOARD ON A340/500-600
. 024
51974
......
31-5012 01
G-VNAP
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G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
INDICATING/RECORDING SYSTEMS - EIS
- INSTALL NEW EIS2 STD L5 TO INCREASE
SYSTEM ROBUSTNESS AND MATURITY
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52465
32-5029
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LANDING GEAR - NORMAL BRAKING INSTALL NEW BSCU WITH HARDWARE DD8 AND
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VALIDITY
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LANDING GEAR-NORMAL BRAKINGINSTALL WIRING FOR FREEFALL SWITCH
MONITOR
ALL
. 025
52652
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EQUIPMENT/FURNISHINGS - CURTAINS AND
PARTITIONS - INSTALL A MAXIMUM NOISE
REDUCED COCKPIT DOOR LOCK SYSTEM (CDLS)
. 025
52845
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G-VSSH
G-VNAP
G-VGAS
G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
INFORMATION SYSTEMS-A/C INFORMATION
NETWORK SYSTEM - INSTALL AINS RESET
COMMAND
. 024A 52866
......
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G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
COMMUNICATIONS - ANTI HIJACK SYSTEM REPLACE HINGE ASSEMBLY FOR THE LCD
SYSTEM CONTROLLER OF THE CDSS
. 025
53389
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G-VGOA
G-VATL
G-VSHY
G-VMEG
G-VFOX
G-VEIL
G-VSSH
G-VWKD
G-VNAP
G-VBLU
G-VGAS
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
INFORMATION SYSTEMS -A/C INFO NETWORK
SYSTEM-INSTALL AINS RESET COMMAND
(SERIAL SOLUTION)
. 025
53923
......
31A5016
G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
INDICATING/RECORDING SYSTEM - EIS:
ACTIVATE CRC MONITORING ON EIS2
ALL
. 025
53951
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...........
INFORMATIONS SYSTEMS - AIRCRAFT
-
INFORMATION NETWORK SYSTEM - REMOVE
AINS/RESET SWITCH AND INOP PLACARD
G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
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FUEL - MAIN FUEL PUMP SYSTEM- INTRODUCE
AN ADDITIONAL THERMAL RELIEF VALVE TO
EACH FUEL LINE
N 025A 54611
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G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
INDICATING/RECORDING SYSTEMS - FWC INSTALL FWC STANDARD W4-1 ON A3456
(WITH 486 CPU BOARD)
N 025A 54624
......
...........
N 025A 54807
28-5033
......
G-VBLU
G-VWIN
G-VFIZ
MSN 0765
G-VFIT
FUEL-FUEL CONTROL AND MONITORING SYSTEM
(FCMS)-AMEND WIRING BETWEEN FDC AND FWC
G-VBLU
G-VWIN
G-VFIZ
MSN 0765
G-VFIT
FUEL-FUEL CONTROL AND MONITORING SYSTEM
(FCMS) - UPDATE FCMC SOFTWARE STANDARD
TO FLIGHTLOAD 8.1
G-VGOA
G-VATL
G-VMEG
G-VOGE
G-VEIL
G-VGAS
G-VWKD
G-VBLU
G-VWIN
G-VFIT
G-VFIZ
MSN 0765
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